Search
Skip to filters
NCAR Aircraft Data Metadata
NCAR Aircraft Data Metadata
SESAME Publications
Data Access
Data Documentation
N304D RAF Data Files for Project SESAME
N304D Sample LRT GENPRO-I header
N304D Sample LRT NetCDF header
N307D RAF Data Files for Project SESAME
Related Links
N304D RAF Data Files for Project SESAME
N304D RAF Data Files for Project SESAME
PRODUCTION MASS STORE BITFILE LOG
Project no.: 1979-443 Project name: Little SESAME
Aircraft: N304D Scientist(s): McCarthy, Ray
Data type: LRT Programmer(s): Mary Dick
Processor used: GENPRO
Output format: GENPRO-I
HPSS path name: /EOL/1979/littlesesame/aircraft/queenaira80_n304d/LRT/GENPRO-I
HPSS file name: Gxxxxx GxxxxxC
MSS format: TBM COS-blocked copies
------------------------------------------------------------------------------
Date Start End File Sizes (Mbytes)
fltno Gxxxxx mm/dd/yyyy Time Time TBM COS-blocked
------------------------------------------------------------------------------
RF01 G50296 04/10/1979 17:05:31 17:56:34 0.737280 0.552960
RF02 G50298 04/13/1979 13:22:02 14:38:33 0.983040 (0.827392)
RF03 G50299 04/17/1979 13:59:22 16:25:21 1.720320 (1.572864)
RF04A G50300 04/19/1979 12:35:52 14:39:00 1.474560 (1.327104)
RF04B G50302 04/19/1979 15:51:57 19:03:26 2.211840 (2.060288)
RF05 G50303 04/25/1979 07:45:18 10:56:25 + +
RF06 G50304 05/02/1979 16:17:21 19:52:15 2.457600 (2.306048)
RF07 G50305 05/07/1979 09:34:48 11:58:06 1.720320 (1.544192)
RF08 G50307 05/14/1979 09:00:04 11:13:23 1.597440 (1.433600)
RF09 G50308 05/16/1979 08:17:49 10:04:36 1.351680 (1.155072)
RF10 G50309 05/18/1979 08:08:50 10:40:45 1.843200 (1.638400)
RF11 G50310 05/21/1979 14:27:11 16:43:26 1.597440 (1.466368)
RF12 G50311 05/24/1979 07:51:34 10:12:24 + +
RF13 G50312 05/26/1979 13:24:30 15:24:54 1.474560 (1.298432)
RF14 G50313 05/27/1979 11:50:00 15:46:47 2.703360 (2.543616)
RF15 G50314 05/30/1979 09:15:04 10:40:35 1.105920 (0.925696)
RF16 G50315 06/01/1979 06:13:20 09:52:15 2.580480 (2.351104)
RF17 G50316 06/04/1979 12:24:07 16:24:59 2.703360 (2.588672)
RF18 G50351 06/06/1979 08:31:35 10:20:04 23.715840 (23.646208)
RF19A G50353 06/06/1979 12:06:38 12:23:04 28.753920* (28.635136)*
RF19B G50353 06/06/1979 12:32:00 14:26:54
RF20 G50317 06/06/1979 15:16:57 18:53:12 2.457600 (2.322432)
RF21 G50318 06/07/1979 09:54:14 13:27:13 2.457600 (2.289664)
RF22 G50319 06/08/1979 09:00:43 12:54:10 2.703360 (2.506752)
RF23 G50320 06/11/1979 12:27:50 14:29:57 1.474560 (1.314816)
------------------------------------------------------------------------------
* Note: Bitfile size includes multiple flight segments.
+ Note: Bitfile missing from SCD Mass Store System archive.
() Note: COS-blocked bitfiles purged by mistake in May 2008
------------------------------------------------------------------------------
SESAME Publications
Data Access
Data Documentation
N304D RAF Data Files for Project SESAME
N304D Sample LRT GENPRO-I header
N304D Sample LRT NetCDF header
N307D RAF Data Files for Project SESAME
Related Links
N304D Sample LRT GENPRO-I header
N304D Sample LRT GENPRO-I header
443-1 LITTLE SESAME 10APR79 17/05/30 FIRST TIME ON THIS FILE 17 5 31 THIS FILE I
S ALL OR PART OF TIME PERIOD 17 5 30 TO 17 56 40 DESCRIPTION OF RECORD -- 71 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 71 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 21 CYCLES OF 71 SAMP/CYC = 1491 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 497 60 BIT PACKED WORDS --METHOD OF SCALING-- A BIAS AD(I) WAS ADDED TO EACH SAMPLE
OF EACH PARAMETER TO ELIMINATE ANY NEGATIVE VALUES. THE BIASED SAMPLE WAS THEN MULTIPLIED BY P(I)
TO INSURE THE PROPER NUMBER OF DECIMAL PLACES WERE SAVED. THE PACKED RECORD MAY BE UNPACKED BY RIGH
T JUSTIFYING 20 BITS AT A TIME AND REVERSING THE ABOVE SCALING PROCESS. AS EXAMPLE, S(I)=N/P(I)-AD(I
), WHERE N IS THE 20 BIT SCALED INTEGER, S(I) THE DESIRED UNSCALED PARAMETER, AD(I),P(I) THE CORRESP
ONDING SCALE FACTORS THE ORDER, RATE, PLOT TITLE, PRINT LAB, UNITS, AD AND P SCALE FACTORS OF EACH
PARAMETER FOLLOW
1) 1 PROCESSOR TIME (SECONDS) AFTER MIDNIGHT TIME SEC = (N/ 1.0) - 0.0
2) 1 UNALTERED TAPE TIME (SEC) AFTER MIDNIGHT TPTIME SEC = (N/ 1.0) - 0.0
3) 1 LTN-51 ARINC TIME LAG (SEC) TMLAG SEC = (N/ 1000.0) - 100.0
4) 1 EVENT MARKER WORD EVMRKS = (N/ 1.0) - 0.0
5) 1 PILOT MICROPHONE SWITCH (XMIT) (VDC) XMIT VDC = (N/ 1000.0) - 100.0
6) 1 FIXED ZERO VOLTAGE (VDC) FZV VDC = (N/ 1000.0) - 100.0
7) 1 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 100.0
8) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
9) 1 AIRCRAFT TRUE HEADING (ARINC) (DEG) THI DEG = (N/ 1000.0) - 100.0
10) 1 INS WANDER ANGLE (DEG) ALPHA DEG = (N/ 1000.0) - 100.0
11) 1 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
12) 1 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
13) 1 RAW INS GROUND SPEED (M/S) GSF M/S = (N/ 1000.0) - 100.0
14) 1 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH DEG = (N/ 1000.0) - 100.0
15) 1 AIRCRAFT ROLL ATTITUDE ANGLE (DEG) ROLL DEG = (N/ 1000.0) - 100.0
16) 1 AIRCRAFT TRUE HEADING (YAW) (DEG) THF DEG = (N/ 1000.0) - 100.0
17) 1 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 1000.0) - 500.0
18) 1 RAW DYNAMIC PRESSURE (WING) (MB) QCW MB = (N/ 1000.0) - 100.0
19) 1 RAW DYNAMIC PRESSURE (GUST PROBE) (MB) QCG MB = (N/ 1000.0) - 100.0
20) 1 CORRECTED DYNAMIC PRESR (WING) (MB) QCWC MB = (N/ 1000.0) - 100.0
21) 1 CORRECTED DYNAMIC PRESR (GUST PROBE)(MB) QCGC MB = (N/ 1000.0) - 100.0
22) 1 RAW STATIC PRESSURE (FUSELAGE) (MB) PSF MB = (N/ 1000.0) - 0.0
23) 1 RAW STATIC PRESSURE (BOOM) (MB) PSB MB = (N/ 1000.0) - 0.0
24) 1 CORRECTED STATIC PRESR (FUSELAGE) (MB) PSFC MB = (N/ 1000.0) - 0.0
25) 1 NACA PRESSURE ALTITUDE (M) HP M = (N/ 10.0) - 500.0
26) 1 GEOMETRIC (RADIO) ALTITUDE (M) HGM M = (N/ 1000.0) - 100.0
27) 1 TOTAL TEMPERATURE (WING ROSEMOUNT) (C) TTW C = (N/ 1000.0) - 100.0
28) 1 TOTAL TEMPERATURE (REVERSE FLOW) (C) TTRF C = (N/ 1000.0) - 100.0
29) 1 TOTAL TEMPERATURE (FAST RESPONSE) (C) TTKP C = (N/ 1000.0) - 100.0
30) 1 AMBIENT TEMPERATURE (ROSEMOUNT) (C) ATW C = (N/ 1000.0) - 100.0
31) 1 AMBIENT TEMPERATURE (REVERSE-FLOW) (C) ATRF C = (N/ 1000.0) - 100.0
32) 1 AMBIENT TEMPERATURE (FAST RESPONSE) (C) ATKP C = (N/ 1000.0) - 100.0
33) 1 RADIOMETRIC SURFACE TEMP (PRT-5) (C) PRT5 C = (N/ 1000.0) - 100.0
34) 1 DEW/FROSTPOINT TEMP (THERMOELEC) (C) DP C = (N/ 1000.0) - 100.0
35) 1 DEWPOINT TEMPERATURE (THERMOELEC) (C) DPC C = (N/ 1000.0) - 100.0
36) 1 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
37) 1 REFRACTIVE INDEX (N-UNITS) RFI N = (N/ 1000.0) - 100.0
38) 1 ABSOLUTE HUMIDITY (REFRACT) (G/M3) RHORF G/M3 = (N/ 1000.0) - 100.0
39) 1 AIRCRAFT TRUE AIRSPEED (WING) (M/S) TASW M/S = (N/ 1000.0) - 100.0
40) 1 AIRCRAFT TRUE AIRSPEED (GUST) (M/S) TASG M/S = (N/ 1000.0) - 100.0
41) 1 RAW J-W LIQUID WATER CONTENT (G/M3) LWC G/M3 = (N/ 1000.0) - 100.0
42) 1 CORRCTD J-W LIQUID WATER CONTENT (G/M3) LWCC G/M3 = (N/ 1000.0) - 100.0
43) 1 ATTACK ANGLE (FIXED VANE) (DEG) AFIX DEG = (N/ 1000.0) - 100.0
44) 1 ATTACK ANGLE (FIXED VANE 2) (DEG) AFIX2 DEG = (N/ 1000.0) - 100.0
45) 1 SIDESLIP ANGLE (FIXED VANE) (DEG) BFIX DEG = (N/ 1000.0) - 100.0
46) 1 SIDESLIP ANGLE (FIXED VANE 2) (DEG) BFIX2 DEG = (N/ 1000.0) - 100.0
47) 1 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 200.0
48) 1 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0
49) 1 WIND VECTOR VERTICAL GUST COMP (H) (M/S) WI M/S = (N/ 1000.0) - 100.0
50) 1 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0
51) 1 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0
52) 1 HORIZONTAL WIND DIRECTION (DEG) WDRCTN DEG = (N/ 1000.0) - 100.0
53) 1 HORIZONTAL WIND SPEED (M/S) WSPD M/S = (N/ 1000.0) - 100.0
54) 1 WIND VECTOR EAST COMPONENT (M/S) UI1 M/S = (N/ 1000.0) - 200.0
55) 1 WIND VECTOR NORTH COMPONENT (M/S) VI1 M/S = (N/ 1000.0) - 200.0
56) 1 WIND VECTOR VERTICAL GUST COMP (L) (M/S) WI1 M/S = (N/ 1000.0) - 100.0
57) 1 WIND VECTOR LNGTDNL COMPONENT (M/S) UX1 M/S = (N/ 1000.0) - 200.0
58) 1 WIND VECTOR LATERAL COMPONENT (M/S) VY1 M/S = (N/ 1000.0) - 200.0
59) 1 RAW INS GROUND SPD EAST COMP (M/S) VEW M/S = (N/ 1000.0) - 500.0
60) 1 RAW INS GROUND SPD NORTH COMP (M/S) VNS M/S = (N/ 1000.0) - 500.0
61) 1 DISTANCE EAST OF NORMAN RADAR (KM) DEI KM = (N/ 10.0) - 5000.0
62) 1 DISTANCE NORTH OF NORMAN RADAR (KM) DNI KM = (N/ 10.0) - 5000.0
63) 1 AIRCRAFT C.G. ACCELERATION (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
64) 1 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP3 M/S = (N/ 1000.0) - 100.0
65) 1 PRESSURE-DAMPED INERTIAL ALTITUDE (M) HI3 M = (N/ 10.0) - 500.0
66) 1 TEMPERATURE AT LIFTING COND. LEVEL (C) TLCL C = (N/ 1000.0) - 100.0
67) 1 PRESR AT LIFTING CONDENSATION LEVEL (MB) PLCL MB = (N/ 1000.0) - 0.0
68) 1 MIXING RATIO (G/KG) RM G/KG = (N/ 1000.0) - 100.0
69) 1 VIRTUAL POTENTIAL TEMPERATURE (K) VTHETA K = (N/ 1000.0) - 100.0
70) 1 EQUIVALENT POTENTIAL TEMPERATURE (K) ETHETA K = (N/ 1000.0) - 100.0
71) 1 POTENTIAL TEMPERATURE (K) THETA K = (N/ 1000.0) - 100.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
443-1 LITTLE SESAME 10APR79 17/05/30
THIS FILE IS ALL OR PART OF THE TIME PERIOD 17 5 30 TO 17 56 40
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
82 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
68224 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 1420 BITS PER LOGICAL DATA RECORD
21 LOGICAL DATA RECORDS PER PHYSICAL RECORD
29820 BITS PER PHYSICAL DATA RECORD
SESAME Publications
Data Access
Data Documentation
N304D RAF Data Files for Project SESAME
N304D Sample LRT GENPRO-I header
N304D Sample LRT NetCDF header
N307D RAF Data Files for Project SESAME
Related Links
N304D Sample LRT NetCDF header
N304D Sample LRT NetCDF header
netcdf RF01.19790410.171444_175157 {
dimensions:
Time = 2234 ;
variables:
int Time(Time) ;
Time:long_name = "time of measurement" ;
Time:units = "seconds since 1979-04-10 00:00:00 +0000" ;
Time:strptime_format = "seconds since %F %T %z" ;
Time:standard_name = "time" ;
float TPTIME(Time) ;
TPTIME:long_name = "UNALTERED TAPE TIME (SEC) AFTER MIDNIGHT" ;
TPTIME:units = "s" ;
TPTIME:actual_range = 62084.f, 64317.f ;
TPTIME:SampledRate = 1 ;
TPTIME:_FillValue = -32767.f ;
float TMLAG(Time) ;
TMLAG:long_name = "LTN-51 ARINC TIME LAG (SEC)" ;
TMLAG:units = "s" ;
TMLAG:actual_range = 0.5800018f, 0.5999985f ;
TMLAG:SampledRate = 1 ;
TMLAG:_FillValue = -32767.f ;
float EVMRKS(Time) ;
EVMRKS:long_name = "EVENT MARKER WORD" ;
EVMRKS:units = "unk" ;
EVMRKS:actual_range = 0.f, 0.f ;
EVMRKS:SampledRate = 1 ;
EVMRKS:_FillValue = -32767.f ;
float XMIT(Time) ;
XMIT:long_name = "PILOT MICROPHONE SWITCH (XMIT) (VDC)" ;
XMIT:units = "Vdc" ;
XMIT:actual_range = 0.001998901f, 8.617996f ;
XMIT:SampledRate = 1 ;
XMIT:_FillValue = -32767.f ;
float FZV(Time) ;
FZV:long_name = "FIXED ZERO VOLTAGE (VDC)" ;
FZV:units = "Vdc" ;
FZV:actual_range = -0.0009994507f, 0.f ;
FZV:SampledRate = 1 ;
FZV:_FillValue = -32767.f ;
float LAT(Time) ;
LAT:long_name = "RAW INS LATITUDE (DEG)" ;
LAT:units = "degree_N" ;
LAT:Category = "Position" ;
LAT:standard_name = "latitude" ;
LAT:valid_range = -90.f, 90.f ;
LAT:actual_range = 34.938f, 35.313f ;
LAT:SampledRate = 1 ;
LAT:_FillValue = -32767.f ;
float LON(Time) ;
LON:long_name = "RAW INS LONGITUDE (DEG)" ;
LON:units = "degree_E" ;
LON:Category = "Position" ;
LON:standard_name = "longitude" ;
LON:valid_range = -180.f, 180.f ;
LON:actual_range = -97.737f, -97.468f ;
LON:SampledRate = 1 ;
LON:_FillValue = -32767.f ;
float THI(Time) ;
THI:long_name = "AIRCRAFT TRUE HEADING (ARINC) (DEG)" ;
THI:units = "degree" ;
THI:actual_range = 0.8690033f, 359.693f ;
THI:SampledRate = 1 ;
THI:_FillValue = -32767.f ;
float ALPHA(Time) ;
ALPHA:long_name = "INS WANDER ANGLE (DEG)" ;
ALPHA:units = "degree" ;
ALPHA:actual_range = 325.197f, 325.353f ;
ALPHA:SampledRate = 1 ;
ALPHA:_FillValue = -32767.f ;
float XVI(Time) ;
XVI:long_name = "RAW INS GROUND SPD X COMPONENT (M/S)" ;
XVI:units = "m/s" ;
XVI:actual_range = -68.31299f, 108.394f ;
XVI:SampledRate = 1 ;
XVI:_FillValue = -32767.f ;
float YVI(Time) ;
YVI:long_name = "RAW INS GROUND SPD Y COMPONENT (M/S)" ;
YVI:units = "m/s" ;
YVI:actual_range = -104.491f, 69.828f ;
YVI:SampledRate = 1 ;
YVI:_FillValue = -32767.f ;
float GSF(Time) ;
GSF:long_name = "RAW INS GROUND SPEED (M/S)" ;
GSF:units = "m/s" ;
GSF:actual_range = 26.703f, 117.864f ;
GSF:SampledRate = 1 ;
GSF:_FillValue = -32767.f ;
float PITCH(Time) ;
PITCH:long_name = "AIRCRAFT PITCH ATTITUDE ANGLE (DEG)" ;
PITCH:units = "degree" ;
PITCH:actual_range = -6.322998f, 11.119f ;
PITCH:SampledRate = 1 ;
PITCH:_FillValue = -32767.f ;
float ROLL(Time) ;
ROLL:long_name = "AIRCRAFT ROLL ATTITUDE ANGLE (DEG)" ;
ROLL:units = "degree" ;
ROLL:actual_range = -42.965f, 27.208f ;
ROLL:SampledRate = 1 ;
ROLL:_FillValue = -32767.f ;
float THF(Time) ;
THF:long_name = "AIRCRAFT TRUE HEADING (YAW) (DEG)" ;
THF:units = "degree" ;
THF:actual_range = 0.1149979f, 359.757f ;
THF:SampledRate = 1 ;
THF:_FillValue = -32767.f ;
float VZI(Time) ;
VZI:long_name = "RAW INS VERTICAL VELOCITY (M/S)" ;
VZI:units = "m/s" ;
VZI:actual_range = -22.79599f, 5.588989f ;
VZI:SampledRate = 1 ;
VZI:_FillValue = -32767.f ;
float QCW(Time) ;
QCW:long_name = "RAW DYNAMIC PRESSURE (WING) (MB)" ;
QCW:units = "hPa" ;
QCW:actual_range = 4.849998f, 41.382f ;
QCW:SampledRate = 1 ;
QCW:_FillValue = -32767.f ;
float QCG(Time) ;
QCG:long_name = "RAW DYNAMIC PRESSURE (GUST PROBE) (MB)" ;
QCG:units = "hPa" ;
QCG:actual_range = 4.364998f, 37.23f ;
QCG:SampledRate = 1 ;
QCG:_FillValue = -32767.f ;
float QCWC(Time) ;
QCWC:long_name = "CORRECTED DYNAMIC PRESR (WING) (MB)" ;
QCWC:units = "hPa" ;
QCWC:actual_range = 5.898003f, 40.022f ;
QCWC:SampledRate = 1 ;
QCWC:_FillValue = -32767.f ;
float QCGC(Time) ;
QCGC:long_name = "CORRECTED DYNAMIC PRESR (GUST PROBE)(MB)" ;
QCGC:units = "hPa" ;
QCGC:actual_range = 5.257004f, 41.241f ;
QCGC:SampledRate = 1 ;
QCGC:_FillValue = -32767.f ;
float PSF(Time) ;
PSF:long_name = "RAW STATIC PRESSURE (FUSELAGE) (MB)" ;
PSF:units = "hPa" ;
PSF:actual_range = 683.306f, 953.91f ;
PSF:SampledRate = 1 ;
PSF:_FillValue = -32767.f ;
float PSB(Time) ;
PSB:long_name = "RAW STATIC PRESSURE (BOOM) (MB)" ;
PSB:units = "hPa" ;
PSB:actual_range = 685.688f, 954.87f ;
PSB:SampledRate = 1 ;
PSB:_FillValue = -32767.f ;
float PSFC(Time) ;
PSFC:long_name = "CORRECTED STATIC PRESR (FUSELAGE) (MB)" ;
PSFC:units = "hPa" ;
PSFC:actual_range = 683.345f, 953.469f ;
PSFC:SampledRate = 1 ;
PSFC:_FillValue = -32767.f ;
float HP(Time) ;
HP:long_name = "NACA PRESSURE ALTITUDE (M)" ;
HP:units = "m" ;
HP:actual_range = 509.7f, 3199.7f ;
HP:SampledRate = 1 ;
HP:_FillValue = -32767.f ;
float HGM(Time) ;
HGM:long_name = "GEOMETRIC (RADIO) ALTITUDE (M)" ;
HGM:units = "m" ;
HGM:actual_range = 0.447998f, 764.253f ;
HGM:SampledRate = 1 ;
HGM:_FillValue = -32767.f ;
float TTW(Time) ;
TTW:long_name = "TOTAL TEMPERATURE (WING ROSEMOUNT) (C)" ;
TTW:units = "deg_C" ;
TTW:actual_range = 3.654999f, 16.222f ;
TTW:SampledRate = 1 ;
TTW:_FillValue = -32767.f ;
float TTRF(Time) ;
TTRF:long_name = "TOTAL TEMPERATURE (REVERSE FLOW) (C)" ;
TTRF:units = "deg_C" ;
TTRF:actual_range = 2.703003f, 14.881f ;
TTRF:SampledRate = 1 ;
TTRF:_FillValue = -32767.f ;
float TTKP(Time) ;
TTKP:long_name = "TOTAL TEMPERATURE (FAST RESPONSE) (C)" ;
TTKP:units = "deg_C" ;
TTKP:actual_range = 3.332001f, 15.207f ;
TTKP:SampledRate = 1 ;
TTKP:_FillValue = -32767.f ;
float ATW(Time) ;
ATW:long_name = "AMBIENT TEMPERATURE (ROSEMOUNT) (C)" ;
ATW:units = "deg_C" ;
ATW:actual_range = 0.8710022f, 13.898f ;
ATW:SampledRate = 1 ;
ATW:_FillValue = -32767.f ;
float ATRF(Time) ;
ATRF:long_name = "AMBIENT TEMPERATURE (REVERSE-FLOW) (C)" ;
ATRF:units = "deg_C" ;
ATRF:actual_range = 0.6930008f, 13.426f ;
ATRF:SampledRate = 1 ;
ATRF:_FillValue = -32767.f ;
float ATKP(Time) ;
ATKP:long_name = "AMBIENT TEMPERATURE (FAST RESPONSE) (C)" ;
ATKP:units = "deg_C" ;
ATKP:actual_range = 0.6959991f, 13.304f ;
ATKP:SampledRate = 1 ;
ATKP:_FillValue = -32767.f ;
float PRT5(Time) ;
PRT5:long_name = "RADIOMETRIC SURFACE TEMP (PRT-5) (C)" ;
PRT5:units = "deg_C" ;
PRT5:actual_range = 8.857002f, 20.702f ;
PRT5:SampledRate = 1 ;
PRT5:_FillValue = -32767.f ;
float DP(Time) ;
DP:long_name = "DEW/FROSTPOINT TEMP (THERMOELEC) (C)" ;
DP:units = "deg_C" ;
DP:actual_range = -11.48f, 13.26f ;
DP:SampledRate = 1 ;
DP:_FillValue = -32767.f ;
float DPC(Time) ;
DPC:long_name = "DEWPOINT TEMPERATURE (THERMOELEC) (C)" ;
DPC:units = "deg_C" ;
DPC:actual_range = -12.874f, 13.26f ;
DPC:SampledRate = 1 ;
DPC:_FillValue = -32767.f ;
float RHOTD(Time) ;
RHOTD:long_name = "ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)" ;
RHOTD:units = "gram/m3" ;
RHOTD:actual_range = 1.779999f, 11.539f ;
RHOTD:SampledRate = 1 ;
RHOTD:_FillValue = -32767.f ;
float RFI(Time) ;
RFI:long_name = "REFRACTIVE INDEX (N-UNITS)" ;
RFI:units = "none" ;
RFI:actual_range = 102.465f, 323.902f ;
RFI:SampledRate = 1 ;
RFI:_FillValue = -32767.f ;
float RHORF(Time) ;
RHORF:long_name = "ABSOLUTE HUMIDITY (REFRACT) (G/M3)" ;
RHORF:units = "gram/m3" ;
RHORF:actual_range = -25.959f, 15.658f ;
RHORF:SampledRate = 1 ;
RHORF:_FillValue = -32767.f ;
float TASW(Time) ;
TASW:long_name = "AIRCRAFT TRUE AIRSPEED (WING) (M/S)" ;
TASW:units = "m/s" ;
TASW:actual_range = 31.883f, 94.464f ;
TASW:SampledRate = 1 ;
TASW:_FillValue = -32767.f ;
float TASG(Time) ;
TASG:long_name = "AIRCRAFT TRUE AIRSPEED (GUST) (M/S)" ;
TASG:units = "m/s" ;
TASG:actual_range = 30.09f, 95.689f ;
TASG:SampledRate = 1 ;
TASG:_FillValue = -32767.f ;
float LWC(Time) ;
LWC:long_name = "RAW J-W LIQUID WATER CONTENT (G/M3)" ;
LWC:units = "gram/m3" ;
LWC:actual_range = -0.7770004f, 0.6750031f ;
LWC:SampledRate = 1 ;
LWC:_FillValue = -32767.f ;
float LWCC(Time) ;
LWCC:long_name = "CORRCTD J-W LIQUID WATER CONTENT (G/M3)" ;
LWCC:units = "gram/m3" ;
LWCC:actual_range = -1.119003f, 0.887001f ;
LWCC:SampledRate = 1 ;
LWCC:_FillValue = -32767.f ;
float AFIX(Time) ;
AFIX:long_name = "ATTACK ANGLE (FIXED VANE) (DEG)" ;
AFIX:units = "degree" ;
AFIX:actual_range = -0.1159973f, 7.357002f ;
AFIX:SampledRate = 1 ;
AFIX:_FillValue = -32767.f ;
float AFIX2(Time) ;
AFIX2:long_name = "ATTACK ANGLE (FIXED VANE 2) (DEG)" ;
AFIX2:units = "degree" ;
AFIX2:actual_range = -1.311996f, 7.133003f ;
AFIX2:SampledRate = 1 ;
AFIX2:_FillValue = -32767.f ;
float BFIX(Time) ;
BFIX:long_name = "SIDESLIP ANGLE (FIXED VANE) (DEG)" ;
BFIX:units = "degree" ;
BFIX:actual_range = -9.473999f, 7.686996f ;
BFIX:SampledRate = 1 ;
BFIX:_FillValue = -32767.f ;
float BFIX2(Time) ;
BFIX2:long_name = "SIDESLIP ANGLE (FIXED VANE 2) (DEG)" ;
BFIX2:units = "degree" ;
BFIX2:actual_range = -7.628998f, 8.777f ;
BFIX2:SampledRate = 1 ;
BFIX2:_FillValue = -32767.f ;
float UI(Time) ;
UI:long_name = "WIND VECTOR EAST GUST COMPONENT (M/S)" ;
UI:units = "m/s" ;
UI:actual_range = -44.925f, 19.873f ;
UI:SampledRate = 1 ;
UI:_FillValue = -32767.f ;
float VI(Time) ;
VI:long_name = "WIND VECTOR NORTH GUST COMPONENT (M/S)" ;
VI:units = "m/s" ;
VI:actual_range = 0.1609955f, 31.224f ;
VI:SampledRate = 1 ;
VI:_FillValue = -32767.f ;
float WI(Time) ;
WI:long_name = "WIND VECTOR VERTICAL GUST COMP (H) (M/S)" ;
WI:units = "m/s" ;
WI:actual_range = -2.009003f, 4.492996f ;
WI:SampledRate = 1 ;
WI:_FillValue = -32767.f ;
float UX(Time) ;
UX:long_name = "WIND VECTOR LNGTDNL GUST COMPONENT (M/S)" ;
UX:units = "m/s" ;
UX:actual_range = -29.535f, 25.371f ;
UX:SampledRate = 1 ;
UX:_FillValue = -32767.f ;
float VY(Time) ;
VY:long_name = "WIND VECTOR LATERAL GUST COMPONENT (M/S)" ;
VY:units = "m/s" ;
VY:actual_range = -47.58299f, 24.464f ;
VY:SampledRate = 1 ;
VY:_FillValue = -32767.f ;
float WDRCTN(Time) ;
WDRCTN:long_name = "HORIZONTAL WIND DIRECTION (DEG)" ;
WDRCTN:units = "degree" ;
WDRCTN:actual_range = 91.29201f, 215.951f ;
WDRCTN:SampledRate = 1 ;
WDRCTN:_FillValue = -32767.f ;
float WSPD(Time) ;
WSPD:long_name = "HORIZONTAL WIND SPEED (M/S)" ;
WSPD:units = "m/s" ;
WSPD:actual_range = 5.360001f, 54.71001f ;
WSPD:SampledRate = 1 ;
WSPD:_FillValue = -32767.f ;
float UI1(Time) ;
UI1:long_name = "WIND VECTOR EAST COMPONENT (M/S)" ;
UI1:units = "m/s" ;
UI1:actual_range = -45.02901f, 20.008f ;
UI1:SampledRate = 1 ;
UI1:_FillValue = -32767.f ;
float VI1(Time) ;
VI1:long_name = "WIND VECTOR NORTH COMPONENT (M/S)" ;
VI1:units = "m/s" ;
VI1:actual_range = -1.085007f, 30.58099f ;
VI1:SampledRate = 1 ;
VI1:_FillValue = -32767.f ;
float WI1(Time) ;
WI1:long_name = "WIND VECTOR VERTICAL GUST COMP (L) (M/S)" ;
WI1:units = "m/s" ;
WI1:actual_range = -2.f, 4.393997f ;
WI1:SampledRate = 1 ;
WI1:_FillValue = -32767.f ;
float UX1(Time) ;
UX1:long_name = "WIND VECTOR LNGTDNL COMPONENT (M/S)" ;
UX1:units = "m/s" ;
UX1:actual_range = -27.47099f, 26.85699f ;
UX1:SampledRate = 1 ;
UX1:_FillValue = -32767.f ;
float VY1(Time) ;
VY1:long_name = "WIND VECTOR LATERAL COMPONENT (M/S)" ;
VY1:units = "m/s" ;
VY1:actual_range = -47.62801f, 24.47301f ;
VY1:SampledRate = 1 ;
VY1:_FillValue = -32767.f ;
float VEW(Time) ;
VEW:long_name = "RAW INS GROUND SPD EAST COMP (M/S)" ;
VEW:units = "m/s" ;
VEW:actual_range = -79.681f, 88.60901f ;
VEW:SampledRate = 1 ;
VEW:_FillValue = -32767.f ;
float VNS(Time) ;
VNS:long_name = "RAW INS GROUND SPD NORTH COMP (M/S)" ;
VNS:units = "m/s" ;
VNS:actual_range = -64.38101f, 116.059f ;
VNS:SampledRate = 1 ;
VNS:_FillValue = -32767.f ;
float DEI(Time) ;
DEI:long_name = "DISTANCE EAST OF NORMAN RADAR (KM)" ;
DEI:units = "km" ;
DEI:actual_range = -24.7998f, -0.3999023f ;
DEI:SampledRate = 1 ;
DEI:_FillValue = -32767.f ;
float DNI(Time) ;
DNI:long_name = "DISTANCE NORTH OF NORMAN RADAR (KM)" ;
DNI:units = "km" ;
DNI:actual_range = -31.8999f, 9.700195f ;
DNI:SampledRate = 1 ;
DNI:_FillValue = -32767.f ;
float CGAC(Time) ;
CGAC:long_name = "AIRCRAFT C.G. ACCELERATION (M/S2)" ;
CGAC:units = "m/s2" ;
CGAC:actual_range = -2.031998f, 1.910004f ;
CGAC:SampledRate = 1 ;
CGAC:_FillValue = -32767.f ;
float WP3(Time) ;
WP3:long_name = "DAMPED AIRCRAFT VERT VELOCITY (M/S)" ;
WP3:units = "m/s" ;
WP3:actual_range = -7.380997f, 6.402f ;
WP3:SampledRate = 1 ;
WP3:_FillValue = -32767.f ;
float HI3(Time) ;
HI3:long_name = "PRESSURE-DAMPED INERTIAL ALTITUDE (M)" ;
HI3:units = "m" ;
HI3:actual_range = 513.8f, 3197.4f ;
HI3:SampledRate = 1 ;
HI3:_FillValue = -32767.f ;
float TLCL(Time) ;
TLCL:long_name = "TEMPERATURE AT LIFTING COND. LEVEL (C)" ;
TLCL:units = "deg_C" ;
TLCL:actual_range = -15.771f, 13.559f ;
TLCL:SampledRate = 1 ;
TLCL:_FillValue = -32767.f ;
float PLCL(Time) ;
PLCL:long_name = "PRESR AT LIFTING CONDENSATION LEVEL (MB)" ;
PLCL:units = "hPa" ;
PLCL:actual_range = 534.514f, 959.611f ;
PLCL:SampledRate = 1 ;
PLCL:_FillValue = -32767.f ;
float RM(Time) ;
RM:long_name = "MIXING RATIO (G/KG)" ;
RM:units = "g/kg" ;
RM:actual_range = 2.07f, 11.265f ;
RM:SampledRate = 1 ;
RM:_FillValue = -32767.f ;
float VTHETA(Time) ;
VTHETA:long_name = "VIRTUAL POTENTIAL TEMPERATURE (K)" ;
VTHETA:units = "deg_K" ;
VTHETA:actual_range = 289.646f, 308.692f ;
VTHETA:SampledRate = 1 ;
VTHETA:_FillValue = -32767.f ;
float ETHETA(Time) ;
ETHETA:long_name = "EQUIVALENT POTENTIAL TEMPERATURE (K)" ;
ETHETA:units = "deg_K" ;
ETHETA:actual_range = 312.052f, 332.11f ;
ETHETA:SampledRate = 1 ;
ETHETA:_FillValue = -32767.f ;
float THETA(Time) ;
THETA:long_name = "POTENTIAL TEMPERATURE (K)" ;
THETA:units = "deg_K" ;
THETA:actual_range = 288.103f, 308.294f ;
THETA:SampledRate = 1 ;
THETA:_FillValue = -32767.f ;
// global attributes:
:institution = "NCAR Research Aviation Facility" ;
:Address = "P.O. Box 3000, Boulder, CO 80307-3000" ;
:creator_url = "http://www.eol.ucar.edu" ;
:Conventions = "NCAR-RAF/nimbus" ;
:ConventionsURL = "http://www.eol.ucar.edu/raf/Software/netCDF.html" ;
:ConventionsVersion = "1.3" ;
:Metadata_Conventions = "Unidata Dataset Discovery v1.0" ;
:standard_name_vocabulary = "CF-1.0" ;
:time_coordinate = "Time" ;
:Phone = "(303) 497-1030" ;
:ProcessorURL = "https://github.com/ncareol/GENPRO" ;
:ProcessorRevision = "8ff1ae2e-dirty" ;
:Categories = "Position,Thermodynamic,Aircraft State,Atmos. State" ;
:geospatial_vertical_positive = "up" ;
:date_created = "2016-08-09T18:37:50 +0000" ;
:Platform = "N304D" ;
:wind_field = "WSPD WDRCTN WI" ;
:time_coverage_start = "1979-04-10T17:14:44 +0000" ;
:time_coverage_end = "1979-04-10T17:51:57 +0000" ;
:TimeInterval = "17:14:44-17:51:57" ;
:FlightDate = "04/10/1979" ;
:geospatial_lat_min = 34.938f ;
:geospatial_lat_max = 35.313f ;
:latitude_coordinate = "LAT" ;
:geospatial_lon_min = -97.737f ;
:geospatial_lon_max = -97.468f ;
:longitude_coordinate = "LON" ;
:zaxis_coordinate = "HP" ;
:geospatial_vertical_units = "m" ;
:geospatial_vertical_min = 509.7f ;
:geospatial_vertical_max = 3199.7f ;
:DESCRIPTION = "443-1 LITTLE SESAME 10APR79 17/05/30" ;
:CYCLE_TIME = 1.f ;
:FlightNumber = "RF01" ;
:ProjectName = "Little SESAME" ;
:converted_from = "G50296" ;
}
SESAME Publications
Data Access
Data Documentation
N304D RAF Data Files for Project SESAME
N304D Sample LRT GENPRO-I header
N304D Sample LRT NetCDF header
N307D RAF Data Files for Project SESAME
Related Links
N307D RAF Data Files for Project SESAME
N307D RAF Data Files for Project SESAME
PRODUCTION MASS STORE BITFILE LOG
Project no.: 1979-743 Project name: Little SESAME
Aircraft: N307D Scientist(s): McCarthy
Data type: LRT Programmer(s): Ron Ruth
Processor used: GENPRO
Output format: GENPRO-I
HPSS path name: /EOL/1979/littlesesame/aircraft/sabreliner_n307d/LRT/GENPRO-I
HPSS file name: Gxxxxx GxxxxxC
MSS format: TBM COS-blocked copies
------------------------------------------------------------------------------
Date Start End File Sizes (Mbytes)
fltno Gxxxxx mm/dd/yyyy Time Time TBM COS-blocked
------------------------------------------------------------------------------
RF01 G52078 05/01/1979 11:06:07 12:50:56 2.088960 1.945600
RF02 G52079 05/02/1979 11:45:21 12:34:15 1.105920 (0.913408)
RF03 G52080 05/02/1979 15:47:49 17:56:28 2.580480 (2.379776)
RF04 G52081 05/02/1979 18:55:00 20:13:34 1.597440 (1.458176)
RF05 G52082 05/03/1979 10:30:22 12:04:16 1.966080 (1.740800)
RF06 G52083 05/07/1979 09:46:06 12:03:00 2.703360 (2.531328)
RF07 G52084 05/09/1979 11:51:41 14:31:10 3.072000 (2.949120)
RF08 G52085 05/14/1979 08:55:10 10:51:16 2.334720 (2.150400)
RF09 G52086 05/16/1979 12:58:16 14:04:15 1.351680 (1.224704)
RF10 G52087 05/17/1979 12:07:07 14:23:51 2.703360 (2.527232)
RF11 G52088 05/18/1979 09:11:18 11:03:47 2.211840 (2.084864)
RF12 G52089 05/18/1979 14:37:06 17:11:15 3.072000 (2.846720)
RF13A G52090 05/19/1979 13:00:00 13:16:35 1.105920* (0.970752*)
RF13B G52090 05/19/1979 13:40:45 14:15:44
RF14 G52093 05/25/1979 13:28:26 15:22:40 2.334720 (2.117632)
RF15 G52094 05/27/1979 11:54:14 14:44:53 3.317760 (3.153920)
RF16 G52095 05/27/1979 15:23:30 17:22:14 2.334720 (2.199552)
RF17 G52096 05/30/1979 09:37:57 11:52:31 2.703360 (2.486272)
RF18 G52101 05/31/1979 05:53:47 08:03:57 2.580480 (2.453504)
------------------------------------------------------------------------------
* Note: Bitfile size includes multiple flight segments.
() Note: COS-blocked bitfiles purged by mistake in May 2008
------------------------------------------------------------------------------
SESAME Publications
Data Access
Data Documentation
N304D RAF Data Files for Project SESAME
N304D Sample LRT GENPRO-I header
N304D Sample LRT NetCDF header
N307D RAF Data Files for Project SESAME
Related Links
N307D Sample LRT GENPRO-I header
N307D Sample LRT GENPRO-I header
743-01 LITTLE SESAME 1 MAY 79 11/06/07 FIRST TIME ON THIS FILE 11 6 7 THIS FILE I
S ALL OR PART OF TIME PERIOD 11 6 7 TO 13 0 0 DESCRIPTION OF RECORD -- 122 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 122 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 12 CYCLES OF 122 SAMP/CYC = 1464 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 488 60 BIT PACKED WORDS --METHOD OF SCALING-- A BIAS AD(I) WAS ADDED TO EACH SAMPLE
OF EACH PARAMETER TO ELIMINATE ANY NEGATIVE VALUES. THE BIASED SAMPLE WAS THEN MULTIPLIED BY P(I)
TO INSURE THE PROPER NUMBER OF DECIMAL PLACES WERE SAVED. THE PACKED RECORD MAY BE UNPACKED BY RIGH
T JUSTIFYING 20 BITS AT A TIME AND REVERSING THE ABOVE SCALING PROCESS. AS EXAMPLE, S(I)=N/P(I)-AD(I
), WHERE N IS THE 20 BIT SCALED INTEGER, S(I) THE DESIRED UNSCALED PARAMETER, AD(I),P(I) THE CORRESP
ONDING SCALE FACTORS THE ORDER, RATE, PLOT TITLE, PRINT LAB, UNITS, AD AND P SCALE FACTORS OF EACH
PARAMETER FOLLOW
1) 1 PROCESSOR TIME (SECONDS) AFTER MIDNIGHT TIME SEC = (N/ 1.0) - 0.0
2) 1 UNALTERED TAPE TIME (SEC) AFTER MIDNIGHT TPTIME SEC = (N/ 1.0) - 0.0
3) 1 LTN-51 ARINC TIME LAG (SEC) TMLAG SEC = (N/ 1000.0) - 100.0
4) 1 EVENT MARKER WORD EVMRKS = (N/ 1.0) - 0.0
5) 1 FIXED ZERO VOLTAGE (VDC) FZV VDC = (N/ 1000.0) - 100.0
6) 1 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 100.0
7) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
8) 1 AIRCRAFT TRUE HEADING (ARINC) (DEG) THI DEG = (N/ 1000.0) - 100.0
9) 1 INS WANDER ANGLE (DEG) ALPHA DEG = (N/ 1000.0) - 100.0
10) 1 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
11) 1 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
12) 1 RAW INS GROUND SPEED (M/S) GSF M/S = (N/ 1000.0) - 100.0
13) 1 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH DEG = (N/ 1000.0) - 100.0
14) 1 AIRCRAFT ROLL ATTITUDE ANGLE (DEG) ROLL DEG = (N/ 1000.0) - 100.0
15) 1 AIRCRAFT TRUE HEADING (YAW) (DEG) THF DEG = (N/ 1000.0) - 100.0
16) 1 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 1000.0) - 500.0
17) 1 RAW DYNAMIC PRESSURE (FUSELAGE) (MB) QCF MB = (N/ 1000.0) - 100.0
18) 1 RAW DYNAMIC PRESSURE (BOOM) (MB) QCB MB = (N/ 1000.0) - 100.0
19) 1 CORRECTED DYNAMIC PRESR (FUSELAGE) (MB) QCFC MB = (N/ 1000.0) - 100.0
20) 1 CORRECTED DYNAMIC PRESSURE (BOOM) (MB) QCBC MB = (N/ 1000.0) - 100.0
21) 1 RAW STATIC PRESSURE (BOOM) (MB) PSB MB = (N/ 1000.0) - 0.0
22) 1 CORRECTED STATIC PRESSURE (BOOM) (MB) PSBC MB = (N/ 1000.0) - 0.0
23) 1 NACA PRESSURE ALTITUDE (M) HP M = (N/ 10.0) - 500.0
24) 1 TOTAL TEMPERATURE (FUS. ROSEMOUNT) (C) TTF C = (N/ 1000.0) - 100.0
25) 1 TOTAL TEMPERATURE (DEICED ROSEMNT) (C) TTFH C = (N/ 1000.0) - 100.0
26) 1 AMBIENT TEMPERATURE (ROSEMOUNT) (C) ATF C = (N/ 1000.0) - 100.0
27) 1 AMBIENT TEMP (DEICED ROSEMOUNT) (C) ATFH C = (N/ 1000.0) - 100.0
28) 1 DEW/FROSTPOINT TEMP (THERMOELEC) (C) DP C = (N/ 1000.0) - 100.0
29) 1 DEWPOINT TEMPERATURE (THERMOELEC) (C) DPC C = (N/ 1000.0) - 100.0
30) 1 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
31) 1 AIRCRAFT TRUE AIRSPEED (FUSELAGE) (M/S) TASF M/S = (N/ 1000.0) - 100.0
32) 1 AIRCRAFT TRUE AIRSPEED (BOOM) (M/S) TASB M/S = (N/ 1000.0) - 100.0
33) 1 VERTICAL DIFF. PRESR (GUST PROBE) (MB) ADIF MB = (N/ 1000.0) - 100.0
34) 1 ATTACK ANGLE (ROSEMOUNT) (DEG) ATTACK DEG = (N/ 1000.0) - 100.0
35) 1 HORIZONTAL DIFF. PRESR (GUST PROBE) (MB) BDIF MB = (N/ 1000.0) - 100.0
36) 1 SIDESLIP ANGLE (ROSEMOUNT) (DEG) SSLIP DEG = (N/ 1000.0) - 100.0
37) 1 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 200.0
38) 1 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0
39) 1 WIND VECTOR VERTICAL GUST COMP (H) (M/S) WI M/S = (N/ 1000.0) - 100.0
40) 1 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0
41) 1 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0
42) 1 HORIZONTAL WIND DIRECTION (DEG) WDRCTN DEG = (N/ 1000.0) - 100.0
43) 1 HORIZONTAL WIND SPEED (M/S) WSPD M/S = (N/ 1000.0) - 100.0
44) 1 WIND VECTOR EAST COMPONENT (M/S) UI1 M/S = (N/ 1000.0) - 200.0
45) 1 WIND VECTOR NORTH COMPONENT (M/S) VI1 M/S = (N/ 1000.0) - 200.0
46) 1 WIND VECTOR LNGTDNL COMPONENT (M/S) UX1 M/S = (N/ 1000.0) - 200.0
47) 1 WIND VECTOR LATERAL COMPONENT (M/S) VY1 M/S = (N/ 1000.0) - 200.0
48) 1 RAW INS GROUND SPD EAST COMP (M/S) VEW M/S = (N/ 1000.0) - 500.0
49) 1 RAW INS GROUND SPD NORTH COMP (M/S) VNS M/S = (N/ 1000.0) - 500.0
50) 1 DISTANCE EAST OF NORMAN RADAR (KM) DEINOR KM = (N/ 10.0) - 5000.0
51) 1 DISTANCE NORTH OF NORMAN RADAR (KM) DNINOR KM = (N/ 10.0) - 5000.0
52) 1 AIRCRAFT C.G. ACCELERATION (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
53) 1 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP3 M/S = (N/ 1000.0) - 100.0
54) 1 PRESSURE-DAMPED INERTIAL ALTITUDE (M) HI3 M = (N/ 10.0) - 500.0
55) 1 POTENTIAL TEMPERATURE (K) THETA K = (N/ 1000.0) - 100.0
56) 1 MIXING RATIO (G/KG) RM G/KG = (N/ 1000.0) - 100.0
57) 1 TEMPERATURE AT LIFTING COND. LEVEL (C) TLCL C = (N/ 1000.0) - 100.0
58) 1 PRESR AT LIFTING CONDENSATION LEVEL (MB) PLCL MB = (N/ 1000.0) - 0.0
59) 1 EQUIVALENT POTENTIAL TEMPERATURE (K) ETHETA K = (N/ 1000.0) - 100.0
60) 1 VIRTUAL POTENTIAL TEMPERATURE (K) VTHETA K = (N/ 1000.0) - 100.0
61) 1 PROBE 1 I. D. -- OAP200X (CLOUD DROPLET) IDPR1 OAP200X = (N/ 1.0) - 0.0
62) 1 PROBE 1/CELL 1 ACCUMULATION (COUNTS) SUM1/ 1 COUNTS = (N/ 1.0) - 0.0
63) 1 PROBE 1/CELL 2 ACCUMULATION (COUNTS) SUM1/ 2 COUNTS = (N/ 1.0) - 0.0
64) 1 PROBE 1/CELL 3 ACCUMULATION (COUNTS) SUM1/ 3 COUNTS = (N/ 1.0) - 0.0
65) 1 PROBE 1/CELL 4 ACCUMULATION (COUNTS) SUM1/ 4 COUNTS = (N/ 1.0) - 0.0
66) 1 PROBE 1/CELL 5 ACCUMULATION (COUNTS) SUM1/ 5 COUNTS = (N/ 1.0) - 0.0
67) 1 PROBE 1/CELL 6 ACCUMULATION (COUNTS) SUM1/ 6 COUNTS = (N/ 1.0) - 0.0
68) 1 PROBE 1/CELL 7 ACCUMULATION (COUNTS) SUM1/ 7 COUNTS = (N/ 1.0) - 0.0
69) 1 PROBE 1/CELL 8 ACCUMULATION (COUNTS) SUM1/ 8 COUNTS = (N/ 1.0) - 0.0
70) 1 PROBE 1/CELL 9 ACCUMULATION (COUNTS) SUM1/ 9 COUNTS = (N/ 1.0) - 0.0
71) 1 PROBE 1/CELL10 ACCUMULATION (COUNTS) SUM1/10 COUNTS = (N/ 1.0) - 0.0
72) 1 PROBE 1/CELL11 ACCUMULATION (COUNTS) SUM1/11 COUNTS = (N/ 1.0) - 0.0
73) 1 PROBE 1/CELL12 ACCUMULATION (COUNTS) SUM1/12 COUNTS = (N/ 1.0) - 0.0
74) 1 PROBE 1/CELL13 ACCUMULATION (COUNTS) SUM1/13 COUNTS = (N/ 1.0) - 0.0
75) 1 PROBE 1/CELL14 ACCUMULATION (COUNTS) SUM1/14 COUNTS = (N/ 1.0) - 0.0
76) 1 PROBE 1/CELL15 ACCUMULATION (COUNTS) SUM1/15 COUNTS = (N/ 1.0) - 0.0
77) 1 PROBE 2 I. D. -- OAP200Y (PRECIP) IDPR2 OAP200Y = (N/ 1.0) - 0.0
78) 1 PROBE 2/CELL 1 ACCUMULATION (COUNTS) SUM2/ 1 COUNTS = (N/ 1.0) - 0.0
79) 1 PROBE 2/CELL 2 ACCUMULATION (COUNTS) SUM2/ 2 COUNTS = (N/ 1.0) - 0.0
80) 1 PROBE 2/CELL 3 ACCUMULATION (COUNTS) SUM2/ 3 COUNTS = (N/ 1.0) - 0.0
81) 1 PROBE 2/CELL 4 ACCUMULATION (COUNTS) SUM2/ 4 COUNTS = (N/ 1.0) - 0.0
82) 1 PROBE 2/CELL 5 ACCUMULATION (COUNTS) SUM2/ 5 COUNTS = (N/ 1.0) - 0.0
83) 1 PROBE 2/CELL 6 ACCUMULATION (COUNTS) SUM2/ 6 COUNTS = (N/ 1.0) - 0.0
84) 1 PROBE 2/CELL 7 ACCUMULATION (COUNTS) SUM2/ 7 COUNTS = (N/ 1.0) - 0.0
85) 1 PROBE 2/CELL 8 ACCUMULATION (COUNTS) SUM2/ 8 COUNTS = (N/ 1.0) - 0.0
86) 1 PROBE 2/CELL 9 ACCUMULATION (COUNTS) SUM2/ 9 COUNTS = (N/ 1.0) - 0.0
87) 1 PROBE 2/CELL10 ACCUMULATION (COUNTS) SUM2/10 COUNTS = (N/ 1.0) - 0.0
88) 1 PROBE 2/CELL11 ACCUMULATION (COUNTS) SUM2/11 COUNTS = (N/ 1.0) - 0.0
89) 1 PROBE 2/CELL12 ACCUMULATION (COUNTS) SUM2/12 COUNTS = (N/ 1.0) - 0.0
90) 1 PROBE 2/CELL13 ACCUMULATION (COUNTS) SUM2/13 COUNTS = (N/ 1.0) - 0.0
91) 1 PROBE 2/CELL14 ACCUMULATION (COUNTS) SUM2/14 COUNTS = (N/ 1.0) - 0.0
92) 1 PROBE 2/CELL15 ACCUMULATION (COUNTS) SUM2/15 COUNTS = (N/ 1.0) - 0.0
93) 1 PROBE 1/CELL 1 CONCENTRATION (N/CM3) CON1/ 1 N/CM3 = (N/ 100.0) - 0.0
94) 1 PROBE 1/CELL 2 CONCENTRATION (N/CM3) CON1/ 2 N/CM3 = (N/ 100.0) - 0.0
95) 1 PROBE 1/CELL 3 CONCENTRATION (N/CM3) CON1/ 3 N/CM3 = (N/ 100.0) - 0.0
96) 1 PROBE 1/CELL 4 CONCENTRATION (N/CM3) CON1/ 4 N/CM3 = (N/ 100.0) - 0.0
97) 1 PROBE 1/CELL 5 CONCENTRATION (N/CM3) CON1/ 5 N/CM3 = (N/ 100.0) - 0.0
98) 1 PROBE 1/CELL 6 CONCENTRATION (N/CM3) CON1/ 6 N/CM3 = (N/ 100.0) - 0.0
99) 1 PROBE 1/CELL 7 CONCENTRATION (N/CM3) CON1/ 7 N/CM3 = (N/ 100.0) - 0.0
100) 1 PROBE 1/CELL 8 CONCENTRATION (N/CM3) CON1/ 8 N/CM3 = (N/ 100.0) - 0.0
101) 1 PROBE 1/CELL 9 CONCENTRATION (N/CM3) CON1/ 9 N/CM3 = (N/ 100.0) - 0.0
102) 1 PROBE 1/CELL 10 CONCENTRATION (N/CM3) CON1/10 N/CM3 = (N/ 100.0) - 0.0
103) 1 PROBE 1/CELL 11 CONCENTRATION (N/CM3) CON1/11 N/CM3 = (N/ 100.0) - 0.0
104) 1 PROBE 1/CELL 12 CONCENTRATION (N/CM3) CON1/12 N/CM3 = (N/ 100.0) - 0.0
105) 1 PROBE 1/CELL 13 CONCENTRATION (N/CM3) CON1/13 N/CM3 = (N/ 100.0) - 0.0
106) 1 PROBE 1/CELL 14 CONCENTRATION (N/CM3) CON1/14 N/CM3 = (N/ 100.0) - 0.0
107) 1 PROBE 1/CELL 15 CONCENTRATION (N/CM3) CON1/15 N/CM3 = (N/ 100.0) - 0.0
108) 1 PROBE 2/CELL 1 CONCENTRATION (N/M3) CON2/ 1 N/M3 = (N/ 1.0) - 0.0
109) 1 PROBE 2/CELL 2 CONCENTRATION (N/M3) CON2/ 2 N/M3 = (N/ 1.0) - 0.0
110) 1 PROBE 2/CELL 3 CONCENTRATION (N/M3) CON2/ 3 N/M3 = (N/ 1.0) - 0.0
111) 1 PROBE 2/CELL 4 CONCENTRATION (N/M3) CON2/ 4 N/M3 = (N/ 1.0) - 0.0
112) 1 PROBE 2/CELL 5 CONCENTRATION (N/M3) CON2/ 5 N/M3 = (N/ 1.0) - 0.0
113) 1 PROBE 2/CELL 6 CONCENTRATION (N/M3) CON2/ 6 N/M3 = (N/ 1.0) - 0.0
114) 1 PROBE 2/CELL 7 CONCENTRATION (N/M3) CON2/ 7 N/M3 = (N/ 1.0) - 0.0
115) 1 PROBE 2/CELL 8 CONCENTRATION (N/M3) CON2/ 8 N/M3 = (N/ 1.0) - 0.0
116) 1 PROBE 2/CELL 9 CONCENTRATION (N/M3) CON2/ 9 N/M3 = (N/ 1.0) - 0.0
117) 1 PROBE 2/CELL 10 CONCENTRATION (N/M3) CON2/10 N/M3 = (N/ 1.0) - 0.0
118) 1 PROBE 2/CELL 11 CONCENTRATION (N/M3) CON2/11 N/M3 = (N/ 1.0) - 0.0
119) 1 PROBE 2/CELL 12 CONCENTRATION (N/M3) CON2/12 N/M3 = (N/ 1.0) - 0.0
120) 1 PROBE 2/CELL 13 CONCENTRATION (N/M3) CON2/13 N/M3 = (N/ 1.0) - 0.0
121) 1 PROBE 2/CELL 14 CONCENTRATION (N/M3) CON2/14 N/M3 = (N/ 1.0) - 0.0
122) 1 PROBE 2/CELL 15 CONCENTRATION (N/M3) CON2/15 N/M3 = (N/ 1.0) - 0.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
743-01 LITTLE SESAME 1 MAY 79 11/06/07
THIS FILE IS ALL OR PART OF THE TIME PERIOD 11 6 7 TO 13 0 0
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
133 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
110656 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 2440 BITS PER LOGICAL DATA RECORD
12 LOGICAL DATA RECORDS PER PHYSICAL RECORD
29280 BITS PER PHYSICAL DATA RECORD
SESAME Publications
Data Access
Data Documentation
N304D RAF Data Files for Project SESAME
N304D Sample LRT GENPRO-I header
N304D Sample LRT NetCDF header
N307D RAF Data Files for Project SESAME
Related Links
N307D Sample LRT NetCDF header
N307D Sample LRT NetCDF header
netcdf RF01.19790501.111156_125056 {
dimensions:
Time = 5941 ;
variables:
int Time(Time) ;
Time:long_name = "time of measurement" ;
Time:units = "seconds since 1979-05-01 00:00:00 +0000" ;
Time:strptime_format = "seconds since %F %T %z" ;
Time:standard_name = "time" ;
float TPTIME(Time) ;
TPTIME:long_name = "UNALTERED TAPE TIME (SEC) AFTER MIDNIGHT" ;
TPTIME:units = "s" ;
TPTIME:actual_range = 40316.f, 46256.f ;
TPTIME:SampledRate = 1 ;
TPTIME:_FillValue = -32767.f ;
float TMLAG(Time) ;
TMLAG:long_name = "LTN-51 ARINC TIME LAG (SEC)" ;
TMLAG:units = "s" ;
TMLAG:actual_range = 0.01999664f, 0.02999878f ;
TMLAG:SampledRate = 1 ;
TMLAG:_FillValue = -32767.f ;
float EVMRKS(Time) ;
EVMRKS:long_name = "EVENT MARKER WORD" ;
EVMRKS:units = "unk" ;
EVMRKS:actual_range = 0.f, 0.f ;
EVMRKS:SampledRate = 1 ;
EVMRKS:_FillValue = -32767.f ;
float FZV(Time) ;
FZV:long_name = "FIXED ZERO VOLTAGE (VDC)" ;
FZV:units = "Vdc" ;
FZV:actual_range = -0.002998352f, -0.001998901f ;
FZV:SampledRate = 1 ;
FZV:_FillValue = -32767.f ;
float LAT(Time) ;
LAT:long_name = "RAW INS LATITUDE (DEG)" ;
LAT:units = "degree_N" ;
LAT:Category = "Position" ;
LAT:standard_name = "latitude" ;
LAT:valid_range = -90.f, 90.f ;
LAT:actual_range = 34.85699f, 35.688f ;
LAT:SampledRate = 1 ;
LAT:_FillValue = -32767.f ;
float LON(Time) ;
LON:long_name = "RAW INS LONGITUDE (DEG)" ;
LON:units = "degree_E" ;
LON:Category = "Position" ;
LON:standard_name = "longitude" ;
LON:valid_range = -180.f, 180.f ;
LON:actual_range = -98.429f, -95.746f ;
LON:SampledRate = 1 ;
LON:_FillValue = -32767.f ;
float THI(Time) ;
THI:long_name = "AIRCRAFT TRUE HEADING (ARINC) (DEG)" ;
THI:units = "degree" ;
THI:actual_range = 0.0739975f, 359.961f ;
THI:SampledRate = 1 ;
THI:_FillValue = -32767.f ;
float ALPHA(Time) ;
ALPHA:long_name = "INS WANDER ANGLE (DEG)" ;
ALPHA:units = "degree" ;
ALPHA:actual_range = 180.913f, 182.462f ;
ALPHA:SampledRate = 1 ;
ALPHA:_FillValue = -32767.f ;
float XVI(Time) ;
XVI:long_name = "RAW INS GROUND SPD X COMPONENT (M/S)" ;
XVI:units = "m/s" ;
XVI:actual_range = -195.837f, 190.083f ;
XVI:SampledRate = 1 ;
XVI:_FillValue = -32767.f ;
float YVI(Time) ;
YVI:long_name = "RAW INS GROUND SPD Y COMPONENT (M/S)" ;
YVI:units = "m/s" ;
YVI:actual_range = -161.131f, 226.053f ;
YVI:SampledRate = 1 ;
YVI:_FillValue = -32767.f ;
float GSF(Time) ;
GSF:long_name = "RAW INS GROUND SPEED (M/S)" ;
GSF:units = "m/s" ;
GSF:actual_range = 27.176f, 229.335f ;
GSF:SampledRate = 1 ;
GSF:_FillValue = -32767.f ;
float PITCH(Time) ;
PITCH:long_name = "AIRCRAFT PITCH ATTITUDE ANGLE (DEG)" ;
PITCH:units = "degree" ;
PITCH:actual_range = -4.747002f, 19.772f ;
PITCH:SampledRate = 1 ;
PITCH:_FillValue = -32767.f ;
float ROLL(Time) ;
ROLL:long_name = "AIRCRAFT ROLL ATTITUDE ANGLE (DEG)" ;
ROLL:units = "degree" ;
ROLL:actual_range = -24.149f, 40.536f ;
ROLL:SampledRate = 1 ;
ROLL:_FillValue = -32767.f ;
float THF(Time) ;
THF:long_name = "AIRCRAFT TRUE HEADING (YAW) (DEG)" ;
THF:units = "degree" ;
THF:actual_range = 0.7770004f, 359.898f ;
THF:SampledRate = 1 ;
THF:_FillValue = -32767.f ;
float VZI(Time) ;
VZI:long_name = "RAW INS VERTICAL VELOCITY (M/S)" ;
VZI:units = "m/s" ;
VZI:actual_range = -141.291f, 20.75897f ;
VZI:SampledRate = 1 ;
VZI:_FillValue = -32767.f ;
float QCF(Time) ;
QCF:long_name = "RAW DYNAMIC PRESSURE (FUSELAGE) (MB)" ;
QCF:units = "hPa" ;
QCF:actual_range = 6.457001f, 120.567f ;
QCF:SampledRate = 1 ;
QCF:_FillValue = -32767.f ;
float QCB(Time) ;
QCB:long_name = "RAW DYNAMIC PRESSURE (BOOM) (MB)" ;
QCB:units = "hPa" ;
QCB:actual_range = 5.866997f, 111.258f ;
QCB:SampledRate = 1 ;
QCB:_FillValue = -32767.f ;
float QCFC(Time) ;
QCFC:long_name = "CORRECTED DYNAMIC PRESR (FUSELAGE) (MB)" ;
QCFC:units = "hPa" ;
QCFC:actual_range = 7.056999f, 115.205f ;
QCFC:SampledRate = 1 ;
QCFC:_FillValue = -32767.f ;
float QCBC(Time) ;
QCBC:long_name = "CORRECTED DYNAMIC PRESSURE (BOOM) (MB)" ;
QCBC:units = "hPa" ;
QCBC:actual_range = 6.162003f, 115.222f ;
QCBC:SampledRate = 1 ;
QCBC:_FillValue = -32767.f ;
float PSB(Time) ;
PSB:long_name = "RAW STATIC PRESSURE (BOOM) (MB)" ;
PSB:units = "hPa" ;
PSB:actual_range = 288.33f, 969.504f ;
PSB:SampledRate = 1 ;
PSB:_FillValue = -32767.f ;
float PSBC(Time) ;
PSBC:long_name = "CORRECTED STATIC PRESSURE (BOOM) (MB)" ;
PSBC:units = "hPa" ;
PSBC:actual_range = 286.242f, 968.755f ;
PSBC:SampledRate = 1 ;
PSBC:_FillValue = -32767.f ;
float HP(Time) ;
HP:long_name = "NACA PRESSURE ALTITUDE (M)" ;
HP:units = "m" ;
HP:actual_range = 377.f, 9472.7f ;
HP:SampledRate = 1 ;
HP:_FillValue = -32767.f ;
float TTF(Time) ;
TTF:long_name = "TOTAL TEMPERATURE (FUS. ROSEMOUNT) (C)" ;
TTF:units = "deg_C" ;
TTF:actual_range = -29.996f, 21.091f ;
TTF:SampledRate = 1 ;
TTF:_FillValue = -32767.f ;
float TTFH(Time) ;
TTFH:long_name = "TOTAL TEMPERATURE (DEICED ROSEMNT) (C)" ;
TTFH:units = "deg_C" ;
TTFH:actual_range = -30.36f, 20.765f ;
TTFH:SampledRate = 1 ;
TTFH:_FillValue = -32767.f ;
float ATF(Time) ;
ATF:long_name = "AMBIENT TEMPERATURE (ROSEMOUNT) (C)" ;
ATF:units = "deg_C" ;
ATF:actual_range = -46.303f, 19.528f ;
ATF:SampledRate = 1 ;
ATF:_FillValue = -32767.f ;
float ATFH(Time) ;
ATFH:long_name = "AMBIENT TEMP (DEICED ROSEMOUNT) (C)" ;
ATFH:units = "deg_C" ;
ATFH:actual_range = -46.546f, 18.114f ;
ATFH:SampledRate = 1 ;
ATFH:_FillValue = -32767.f ;
float DP(Time) ;
DP:long_name = "DEW/FROSTPOINT TEMP (THERMOELEC) (C)" ;
DP:units = "deg_C" ;
DP:actual_range = -48.965f, 14.011f ;
DP:SampledRate = 1 ;
DP:_FillValue = -32767.f ;
float DPC(Time) ;
DPC:long_name = "DEWPOINT TEMPERATURE (THERMOELEC) (C)" ;
DPC:units = "deg_C" ;
DPC:actual_range = -53.032f, 14.011f ;
DPC:SampledRate = 1 ;
DPC:_FillValue = -32767.f ;
float RHOTD(Time) ;
RHOTD:long_name = "ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)" ;
RHOTD:units = "gram/m3" ;
RHOTD:actual_range = 0.04100037f, 11.835f ;
RHOTD:SampledRate = 1 ;
RHOTD:_FillValue = -32767.f ;
float TASF(Time) ;
TASF:long_name = "AIRCRAFT TRUE AIRSPEED (FUSELAGE) (M/S)" ;
TASF:units = "m/s" ;
TASF:actual_range = 34.89999f, 198.726f ;
TASF:SampledRate = 1 ;
TASF:_FillValue = -32767.f ;
float TASB(Time) ;
TASB:long_name = "AIRCRAFT TRUE AIRSPEED (BOOM) (M/S)" ;
TASB:units = "m/s" ;
TASB:actual_range = 32.608f, 197.648f ;
TASB:SampledRate = 1 ;
TASB:_FillValue = -32767.f ;
float ADIF(Time) ;
ADIF:long_name = "VERTICAL DIFF. PRESR (GUST PROBE) (MB)" ;
ADIF:units = "hPa" ;
ADIF:actual_range = 0.8700027f, 37.40601f ;
ADIF:SampledRate = 1 ;
ADIF:_FillValue = -32767.f ;
float ATTACK(Time) ;
ATTACK:long_name = "ATTACK ANGLE (ROSEMOUNT) (DEG)" ;
ATTACK:units = "degree" ;
ATTACK:actual_range = 1.255997f, 13.068f ;
ATTACK:SampledRate = 1 ;
ATTACK:_FillValue = -32767.f ;
float BDIF(Time) ;
BDIF:long_name = "HORIZONTAL DIFF. PRESR (GUST PROBE) (MB)" ;
BDIF:units = "hPa" ;
BDIF:actual_range = -25.05f, 40.304f ;
BDIF:SampledRate = 1 ;
BDIF:_FillValue = -32767.f ;
float SSLIP(Time) ;
SSLIP:long_name = "SIDESLIP ANGLE (ROSEMOUNT) (DEG)" ;
SSLIP:units = "degree" ;
SSLIP:actual_range = -4.677002f, 5.767998f ;
SSLIP:SampledRate = 1 ;
SSLIP:_FillValue = -32767.f ;
float UI(Time) ;
UI:long_name = "WIND VECTOR EAST GUST COMPONENT (M/S)" ;
UI:units = "m/s" ;
UI:actual_range = -3.488998f, 36.817f ;
UI:SampledRate = 1 ;
UI:_FillValue = -32767.f ;
float VI(Time) ;
VI:long_name = "WIND VECTOR NORTH GUST COMPONENT (M/S)" ;
VI:units = "m/s" ;
VI:actual_range = -6.796005f, 12.56799f ;
VI:SampledRate = 1 ;
VI:_FillValue = -32767.f ;
float WI(Time) ;
WI:long_name = "WIND VECTOR VERTICAL GUST COMP (H) (M/S)" ;
WI:units = "m/s" ;
WI:actual_range = -1.795998f, 2.420998f ;
WI:SampledRate = 1 ;
WI:_FillValue = -32767.f ;
float UX(Time) ;
UX:long_name = "WIND VECTOR LNGTDNL GUST COMPONENT (M/S)" ;
UX:units = "m/s" ;
UX:actual_range = -30.97099f, 34.377f ;
UX:SampledRate = 1 ;
UX:_FillValue = -32767.f ;
float VY(Time) ;
VY:long_name = "WIND VECTOR LATERAL GUST COMPONENT (M/S)" ;
VY:units = "m/s" ;
VY:actual_range = -32.765f, 35.522f ;
VY:SampledRate = 1 ;
VY:_FillValue = -32767.f ;
float WDRCTN(Time) ;
WDRCTN:long_name = "HORIZONTAL WIND DIRECTION (DEG)" ;
WDRCTN:units = "degree" ;
WDRCTN:actual_range = 139.049f, 301.005f ;
WDRCTN:SampledRate = 1 ;
WDRCTN:_FillValue = -32767.f ;
float WSPD(Time) ;
WSPD:long_name = "HORIZONTAL WIND SPEED (M/S)" ;
WSPD:units = "m/s" ;
WSPD:actual_range = 2.669998f, 41.59f ;
WSPD:SampledRate = 1 ;
WSPD:_FillValue = -32767.f ;
float UI1(Time) ;
UI1:long_name = "WIND VECTOR EAST COMPONENT (M/S)" ;
UI1:units = "m/s" ;
UI1:actual_range = -3.307007f, 38.05901f ;
UI1:SampledRate = 1 ;
UI1:_FillValue = -32767.f ;
float VI1(Time) ;
VI1:long_name = "WIND VECTOR NORTH COMPONENT (M/S)" ;
VI1:units = "m/s" ;
VI1:actual_range = -16.769f, 12.502f ;
VI1:SampledRate = 1 ;
VI1:_FillValue = -32767.f ;
float UX1(Time) ;
UX1:long_name = "WIND VECTOR LNGTDNL COMPONENT (M/S)" ;
UX1:units = "m/s" ;
UX1:actual_range = -35.17101f, 31.617f ;
UX1:SampledRate = 1 ;
UX1:_FillValue = -32767.f ;
float VY1(Time) ;
VY1:long_name = "WIND VECTOR LATERAL COMPONENT (M/S)" ;
VY1:units = "m/s" ;
VY1:actual_range = -35.01199f, 36.70399f ;
VY1:SampledRate = 1 ;
VY1:_FillValue = -32767.f ;
float VEW(Time) ;
VEW:long_name = "RAW INS GROUND SPD EAST COMP (M/S)" ;
VEW:units = "m/s" ;
VEW:actual_range = -162.184f, 226.055f ;
VEW:SampledRate = 1 ;
VEW:_FillValue = -32767.f ;
float VNS(Time) ;
VNS:long_name = "RAW INS GROUND SPD NORTH COMP (M/S)" ;
VNS:units = "m/s" ;
VNS:actual_range = -191.519f, 194.563f ;
VNS:SampledRate = 1 ;
VNS:_FillValue = -32767.f ;
float DEINOR(Time) ;
DEINOR:long_name = "DISTANCE EAST OF NORMAN RADAR (KM)" ;
DEINOR:units = "km" ;
DEINOR:actual_range = -87.6001f, 156.7002f ;
DEINOR:SampledRate = 1 ;
DEINOR:_FillValue = -32767.f ;
float DNINOR(Time) ;
DNINOR:long_name = "DISTANCE NORTH OF NORMAN RADAR (KM)" ;
DNINOR:units = "km" ;
DNINOR:actual_range = -40.7002f, 51.7002f ;
DNINOR:SampledRate = 1 ;
DNINOR:_FillValue = -32767.f ;
float CGAC(Time) ;
CGAC:long_name = "AIRCRAFT C.G. ACCELERATION (M/S2)" ;
CGAC:units = "m/s2" ;
CGAC:actual_range = -4.552002f, 6.003998f ;
CGAC:SampledRate = 1 ;
CGAC:_FillValue = -32767.f ;
float WP3(Time) ;
WP3:long_name = "DAMPED AIRCRAFT VERT VELOCITY (M/S)" ;
WP3:units = "m/s" ;
WP3:actual_range = -26.742f, 19.407f ;
WP3:SampledRate = 1 ;
WP3:_FillValue = -32767.f ;
float HI3(Time) ;
HI3:long_name = "PRESSURE-DAMPED INERTIAL ALTITUDE (M)" ;
HI3:units = "m" ;
HI3:actual_range = 377.1f, 9472.3f ;
HI3:SampledRate = 1 ;
HI3:_FillValue = -32767.f ;
float THETA(Time) ;
THETA:long_name = "POTENTIAL TEMPERATURE (K)" ;
THETA:units = "deg_K" ;
THETA:actual_range = 294.105f, 327.685f ;
THETA:SampledRate = 1 ;
THETA:_FillValue = -32767.f ;
float RM(Time) ;
RM:long_name = "MIXING RATIO (G/KG)" ;
RM:units = "g/kg" ;
RM:actual_range = 0.09200287f, 10.442f ;
RM:SampledRate = 1 ;
RM:_FillValue = -32767.f ;
float TLCL(Time) ;
TLCL:long_name = "TEMPERATURE AT LIFTING COND. LEVEL (C)" ;
TLCL:units = "deg_C" ;
TLCL:actual_range = -53.905f, 12.839f ;
TLCL:SampledRate = 1 ;
TLCL:_FillValue = -32767.f ;
float PLCL(Time) ;
PLCL:long_name = "PRESR AT LIFTING CONDENSATION LEVEL (MB)" ;
PLCL:units = "hPa" ;
PLCL:actual_range = 255.148f, 904.326f ;
PLCL:SampledRate = 1 ;
PLCL:_FillValue = -32767.f ;
float ETHETA(Time) ;
ETHETA:long_name = "EQUIVALENT POTENTIAL TEMPERATURE (K)" ;
ETHETA:units = "deg_K" ;
ETHETA:actual_range = 315.571f, 328.433f ;
ETHETA:SampledRate = 1 ;
ETHETA:_FillValue = -32767.f ;
float VTHETA(Time) ;
VTHETA:long_name = "VIRTUAL POTENTIAL TEMPERATURE (K)" ;
VTHETA:units = "deg_K" ;
VTHETA:actual_range = 294.105f, 327.685f ;
VTHETA:SampledRate = 1 ;
VTHETA:_FillValue = -32767.f ;
float IDPR1(Time) ;
IDPR1:long_name = "PROBE 1 I. D. -- OAP200X (CLOUD DROPLET)" ;
IDPR1:units = "OAP200X" ;
IDPR1:actual_range = 13107.f, 13107.f ;
IDPR1:SampledRate = 1 ;
IDPR1:_FillValue = -32767.f ;
float SUM1_1(Time) ;
SUM1_1:long_name = "PROBE 1/CELL 1 ACCUMULATION (COUNTS)" ;
SUM1_1:units = "COUNTS" ;
SUM1_1:actual_range = 0.f, 3.f ;
SUM1_1:SampledRate = 1 ;
SUM1_1:_FillValue = -32767.f ;
float SUM1_2(Time) ;
SUM1_2:long_name = "PROBE 1/CELL 2 ACCUMULATION (COUNTS)" ;
SUM1_2:units = "COUNTS" ;
SUM1_2:actual_range = 0.f, 5.f ;
SUM1_2:SampledRate = 1 ;
SUM1_2:_FillValue = -32767.f ;
float SUM1_3(Time) ;
SUM1_3:long_name = "PROBE 1/CELL 3 ACCUMULATION (COUNTS)" ;
SUM1_3:units = "COUNTS" ;
SUM1_3:actual_range = 0.f, 6.f ;
SUM1_3:SampledRate = 1 ;
SUM1_3:_FillValue = -32767.f ;
float SUM1_4(Time) ;
SUM1_4:long_name = "PROBE 1/CELL 4 ACCUMULATION (COUNTS)" ;
SUM1_4:units = "COUNTS" ;
SUM1_4:actual_range = 0.f, 6.f ;
SUM1_4:SampledRate = 1 ;
SUM1_4:_FillValue = -32767.f ;
float SUM1_5(Time) ;
SUM1_5:long_name = "PROBE 1/CELL 5 ACCUMULATION (COUNTS)" ;
SUM1_5:units = "COUNTS" ;
SUM1_5:actual_range = 0.f, 9.f ;
SUM1_5:SampledRate = 1 ;
SUM1_5:_FillValue = -32767.f ;
float SUM1_6(Time) ;
SUM1_6:long_name = "PROBE 1/CELL 6 ACCUMULATION (COUNTS)" ;
SUM1_6:units = "COUNTS" ;
SUM1_6:actual_range = 0.f, 11.f ;
SUM1_6:SampledRate = 1 ;
SUM1_6:_FillValue = -32767.f ;
float SUM1_7(Time) ;
SUM1_7:long_name = "PROBE 1/CELL 7 ACCUMULATION (COUNTS)" ;
SUM1_7:units = "COUNTS" ;
SUM1_7:actual_range = 0.f, 14.f ;
SUM1_7:SampledRate = 1 ;
SUM1_7:_FillValue = -32767.f ;
float SUM1_8(Time) ;
SUM1_8:long_name = "PROBE 1/CELL 8 ACCUMULATION (COUNTS)" ;
SUM1_8:units = "COUNTS" ;
SUM1_8:actual_range = 0.f, 12.f ;
SUM1_8:SampledRate = 1 ;
SUM1_8:_FillValue = -32767.f ;
float SUM1_9(Time) ;
SUM1_9:long_name = "PROBE 1/CELL 9 ACCUMULATION (COUNTS)" ;
SUM1_9:units = "COUNTS" ;
SUM1_9:actual_range = 0.f, 12.f ;
SUM1_9:SampledRate = 1 ;
SUM1_9:_FillValue = -32767.f ;
float SUM1_10(Time) ;
SUM1_10:long_name = "PROBE 1/CELL10 ACCUMULATION (COUNTS)" ;
SUM1_10:units = "COUNTS" ;
SUM1_10:actual_range = 0.f, 11.f ;
SUM1_10:SampledRate = 1 ;
SUM1_10:_FillValue = -32767.f ;
float SUM1_11(Time) ;
SUM1_11:long_name = "PROBE 1/CELL11 ACCUMULATION (COUNTS)" ;
SUM1_11:units = "COUNTS" ;
SUM1_11:actual_range = 0.f, 12.f ;
SUM1_11:SampledRate = 1 ;
SUM1_11:_FillValue = -32767.f ;
float SUM1_12(Time) ;
SUM1_12:long_name = "PROBE 1/CELL12 ACCUMULATION (COUNTS)" ;
SUM1_12:units = "COUNTS" ;
SUM1_12:actual_range = 0.f, 10.f ;
SUM1_12:SampledRate = 1 ;
SUM1_12:_FillValue = -32767.f ;
float SUM1_13(Time) ;
SUM1_13:long_name = "PROBE 1/CELL13 ACCUMULATION (COUNTS)" ;
SUM1_13:units = "COUNTS" ;
SUM1_13:actual_range = 0.f, 7.f ;
SUM1_13:SampledRate = 1 ;
SUM1_13:_FillValue = -32767.f ;
float SUM1_14(Time) ;
SUM1_14:long_name = "PROBE 1/CELL14 ACCUMULATION (COUNTS)" ;
SUM1_14:units = "COUNTS" ;
SUM1_14:actual_range = 0.f, 6.f ;
SUM1_14:SampledRate = 1 ;
SUM1_14:_FillValue = -32767.f ;
float SUM1_15(Time) ;
SUM1_15:long_name = "PROBE 1/CELL15 ACCUMULATION (COUNTS)" ;
SUM1_15:units = "COUNTS" ;
SUM1_15:actual_range = 0.f, 5.f ;
SUM1_15:SampledRate = 1 ;
SUM1_15:_FillValue = -32767.f ;
float IDPR2(Time) ;
IDPR2:long_name = "PROBE 2 I. D. -- OAP200Y (PRECIP)" ;
IDPR2:units = "OAP200Y" ;
IDPR2:actual_range = 0.f, 21.f ;
IDPR2:SampledRate = 1 ;
IDPR2:_FillValue = -32767.f ;
float SUM2_1(Time) ;
SUM2_1:long_name = "PROBE 2/CELL 1 ACCUMULATION (COUNTS)" ;
SUM2_1:units = "COUNTS" ;
SUM2_1:actual_range = 0.f, 124.f ;
SUM2_1:SampledRate = 1 ;
SUM2_1:_FillValue = -32767.f ;
float SUM2_2(Time) ;
SUM2_2:long_name = "PROBE 2/CELL 2 ACCUMULATION (COUNTS)" ;
SUM2_2:units = "COUNTS" ;
SUM2_2:actual_range = 0.f, 5.f ;
SUM2_2:SampledRate = 1 ;
SUM2_2:_FillValue = -32767.f ;
float SUM2_3(Time) ;
SUM2_3:long_name = "PROBE 2/CELL 3 ACCUMULATION (COUNTS)" ;
SUM2_3:units = "COUNTS" ;
SUM2_3:actual_range = 0.f, 1.f ;
SUM2_3:SampledRate = 1 ;
SUM2_3:_FillValue = -32767.f ;
float SUM2_4(Time) ;
SUM2_4:long_name = "PROBE 2/CELL 4 ACCUMULATION (COUNTS)" ;
SUM2_4:units = "COUNTS" ;
SUM2_4:actual_range = 0.f, 0.f ;
SUM2_4:SampledRate = 1 ;
SUM2_4:_FillValue = -32767.f ;
float SUM2_5(Time) ;
SUM2_5:long_name = "PROBE 2/CELL 5 ACCUMULATION (COUNTS)" ;
SUM2_5:units = "COUNTS" ;
SUM2_5:actual_range = 0.f, 0.f ;
SUM2_5:SampledRate = 1 ;
SUM2_5:_FillValue = -32767.f ;
float SUM2_6(Time) ;
SUM2_6:long_name = "PROBE 2/CELL 6 ACCUMULATION (COUNTS)" ;
SUM2_6:units = "COUNTS" ;
SUM2_6:actual_range = 0.f, 0.f ;
SUM2_6:SampledRate = 1 ;
SUM2_6:_FillValue = -32767.f ;
float SUM2_7(Time) ;
SUM2_7:long_name = "PROBE 2/CELL 7 ACCUMULATION (COUNTS)" ;
SUM2_7:units = "COUNTS" ;
SUM2_7:actual_range = 0.f, 0.f ;
SUM2_7:SampledRate = 1 ;
SUM2_7:_FillValue = -32767.f ;
float SUM2_8(Time) ;
SUM2_8:long_name = "PROBE 2/CELL 8 ACCUMULATION (COUNTS)" ;
SUM2_8:units = "COUNTS" ;
SUM2_8:actual_range = 0.f, 0.f ;
SUM2_8:SampledRate = 1 ;
SUM2_8:_FillValue = -32767.f ;
float SUM2_9(Time) ;
SUM2_9:long_name = "PROBE 2/CELL 9 ACCUMULATION (COUNTS)" ;
SUM2_9:units = "COUNTS" ;
SUM2_9:actual_range = 0.f, 0.f ;
SUM2_9:SampledRate = 1 ;
SUM2_9:_FillValue = -32767.f ;
float SUM2_10(Time) ;
SUM2_10:long_name = "PROBE 2/CELL10 ACCUMULATION (COUNTS)" ;
SUM2_10:units = "COUNTS" ;
SUM2_10:actual_range = 0.f, 0.f ;
SUM2_10:SampledRate = 1 ;
SUM2_10:_FillValue = -32767.f ;
float SUM2_11(Time) ;
SUM2_11:long_name = "PROBE 2/CELL11 ACCUMULATION (COUNTS)" ;
SUM2_11:units = "COUNTS" ;
SUM2_11:actual_range = 0.f, 0.f ;
SUM2_11:SampledRate = 1 ;
SUM2_11:_FillValue = -32767.f ;
float SUM2_12(Time) ;
SUM2_12:long_name = "PROBE 2/CELL12 ACCUMULATION (COUNTS)" ;
SUM2_12:units = "COUNTS" ;
SUM2_12:actual_range = 0.f, 0.f ;
SUM2_12:SampledRate = 1 ;
SUM2_12:_FillValue = -32767.f ;
float SUM2_13(Time) ;
SUM2_13:long_name = "PROBE 2/CELL13 ACCUMULATION (COUNTS)" ;
SUM2_13:units = "COUNTS" ;
SUM2_13:actual_range = 0.f, 0.f ;
SUM2_13:SampledRate = 1 ;
SUM2_13:_FillValue = -32767.f ;
float SUM2_14(Time) ;
SUM2_14:long_name = "PROBE 2/CELL14 ACCUMULATION (COUNTS)" ;
SUM2_14:units = "COUNTS" ;
SUM2_14:actual_range = 0.f, 0.f ;
SUM2_14:SampledRate = 1 ;
SUM2_14:_FillValue = -32767.f ;
float SUM2_15(Time) ;
SUM2_15:long_name = "PROBE 2/CELL15 ACCUMULATION (COUNTS)" ;
SUM2_15:units = "COUNTS" ;
SUM2_15:actual_range = 0.f, 0.f ;
SUM2_15:SampledRate = 1 ;
SUM2_15:_FillValue = -32767.f ;
float CON1_1(Time) ;
CON1_1:long_name = "PROBE 1/CELL 1 CONCENTRATION (N/CM3)" ;
CON1_1:units = "N/CM3" ;
CON1_1:actual_range = 0.f, 0.21f ;
CON1_1:SampledRate = 1 ;
CON1_1:_FillValue = -32767.f ;
float CON1_2(Time) ;
CON1_2:long_name = "PROBE 1/CELL 2 CONCENTRATION (N/CM3)" ;
CON1_2:units = "N/CM3" ;
CON1_2:actual_range = 0.f, 0.03f ;
CON1_2:SampledRate = 1 ;
CON1_2:_FillValue = -32767.f ;
float CON1_3(Time) ;
CON1_3:long_name = "PROBE 1/CELL 3 CONCENTRATION (N/CM3)" ;
CON1_3:units = "N/CM3" ;
CON1_3:actual_range = 0.f, 0.01f ;
CON1_3:SampledRate = 1 ;
CON1_3:_FillValue = -32767.f ;
float CON1_4(Time) ;
CON1_4:long_name = "PROBE 1/CELL 4 CONCENTRATION (N/CM3)" ;
CON1_4:units = "N/CM3" ;
CON1_4:actual_range = 0.f, 0.01f ;
CON1_4:SampledRate = 1 ;
CON1_4:_FillValue = -32767.f ;
float CON1_5(Time) ;
CON1_5:long_name = "PROBE 1/CELL 5 CONCENTRATION (N/CM3)" ;
CON1_5:units = "N/CM3" ;
CON1_5:actual_range = 0.f, 0.01f ;
CON1_5:SampledRate = 1 ;
CON1_5:_FillValue = -32767.f ;
float CON1_6(Time) ;
CON1_6:long_name = "PROBE 1/CELL 6 CONCENTRATION (N/CM3)" ;
CON1_6:units = "N/CM3" ;
CON1_6:actual_range = 0.f, 0.f ;
CON1_6:SampledRate = 1 ;
CON1_6:_FillValue = -32767.f ;
float CON1_7(Time) ;
CON1_7:long_name = "PROBE 1/CELL 7 CONCENTRATION (N/CM3)" ;
CON1_7:units = "N/CM3" ;
CON1_7:actual_range = 0.f, 0.f ;
CON1_7:SampledRate = 1 ;
CON1_7:_FillValue = -32767.f ;
float CON1_8(Time) ;
CON1_8:long_name = "PROBE 1/CELL 8 CONCENTRATION (N/CM3)" ;
CON1_8:units = "N/CM3" ;
CON1_8:actual_range = 0.f, 0.f ;
CON1_8:SampledRate = 1 ;
CON1_8:_FillValue = -32767.f ;
float CON1_9(Time) ;
CON1_9:long_name = "PROBE 1/CELL 9 CONCENTRATION (N/CM3)" ;
CON1_9:units = "N/CM3" ;
CON1_9:actual_range = 0.f, 0.f ;
CON1_9:SampledRate = 1 ;
CON1_9:_FillValue = -32767.f ;
float CON1_10(Time) ;
CON1_10:long_name = "PROBE 1/CELL 10 CONCENTRATION (N/CM3)" ;
CON1_10:units = "N/CM3" ;
CON1_10:actual_range = 0.f, 0.f ;
CON1_10:SampledRate = 1 ;
CON1_10:_FillValue = -32767.f ;
float CON1_11(Time) ;
CON1_11:long_name = "PROBE 1/CELL 11 CONCENTRATION (N/CM3)" ;
CON1_11:units = "N/CM3" ;
CON1_11:actual_range = 0.f, 0.f ;
CON1_11:SampledRate = 1 ;
CON1_11:_FillValue = -32767.f ;
float CON1_12(Time) ;
CON1_12:long_name = "PROBE 1/CELL 12 CONCENTRATION (N/CM3)" ;
CON1_12:units = "N/CM3" ;
CON1_12:actual_range = 0.f, 0.f ;
CON1_12:SampledRate = 1 ;
CON1_12:_FillValue = -32767.f ;
float CON1_13(Time) ;
CON1_13:long_name = "PROBE 1/CELL 13 CONCENTRATION (N/CM3)" ;
CON1_13:units = "N/CM3" ;
CON1_13:actual_range = 0.f, 0.f ;
CON1_13:SampledRate = 1 ;
CON1_13:_FillValue = -32767.f ;
float CON1_14(Time) ;
CON1_14:long_name = "PROBE 1/CELL 14 CONCENTRATION (N/CM3)" ;
CON1_14:units = "N/CM3" ;
CON1_14:actual_range = 0.f, 0.f ;
CON1_14:SampledRate = 1 ;
CON1_14:_FillValue = -32767.f ;
float CON1_15(Time) ;
CON1_15:long_name = "PROBE 1/CELL 15 CONCENTRATION (N/CM3)" ;
CON1_15:units = "N/CM3" ;
CON1_15:actual_range = 0.f, 0.f ;
CON1_15:SampledRate = 1 ;
CON1_15:_FillValue = -32767.f ;
float CON2_1(Time) ;
CON2_1:long_name = "PROBE 2/CELL 1 CONCENTRATION (N/M3)" ;
CON2_1:units = "N/M3" ;
CON2_1:actual_range = 0.f, 1870.f ;
CON2_1:SampledRate = 1 ;
CON2_1:_FillValue = -32767.f ;
float CON2_2(Time) ;
CON2_2:long_name = "PROBE 2/CELL 2 CONCENTRATION (N/M3)" ;
CON2_2:units = "N/M3" ;
CON2_2:actual_range = 0.f, 28.f ;
CON2_2:SampledRate = 1 ;
CON2_2:_FillValue = -32767.f ;
float CON2_3(Time) ;
CON2_3:long_name = "PROBE 2/CELL 3 CONCENTRATION (N/M3)" ;
CON2_3:units = "N/M3" ;
CON2_3:actual_range = 0.f, 6.f ;
CON2_3:SampledRate = 1 ;
CON2_3:_FillValue = -32767.f ;
float CON2_4(Time) ;
CON2_4:long_name = "PROBE 2/CELL 4 CONCENTRATION (N/M3)" ;
CON2_4:units = "N/M3" ;
CON2_4:actual_range = 0.f, 0.f ;
CON2_4:SampledRate = 1 ;
CON2_4:_FillValue = -32767.f ;
float CON2_5(Time) ;
CON2_5:long_name = "PROBE 2/CELL 5 CONCENTRATION (N/M3)" ;
CON2_5:units = "N/M3" ;
CON2_5:actual_range = 0.f, 0.f ;
CON2_5:SampledRate = 1 ;
CON2_5:_FillValue = -32767.f ;
float CON2_6(Time) ;
CON2_6:long_name = "PROBE 2/CELL 6 CONCENTRATION (N/M3)" ;
CON2_6:units = "N/M3" ;
CON2_6:actual_range = 0.f, 0.f ;
CON2_6:SampledRate = 1 ;
CON2_6:_FillValue = -32767.f ;
float CON2_7(Time) ;
CON2_7:long_name = "PROBE 2/CELL 7 CONCENTRATION (N/M3)" ;
CON2_7:units = "N/M3" ;
CON2_7:actual_range = 0.f, 0.f ;
CON2_7:SampledRate = 1 ;
CON2_7:_FillValue = -32767.f ;
float CON2_8(Time) ;
CON2_8:long_name = "PROBE 2/CELL 8 CONCENTRATION (N/M3)" ;
CON2_8:units = "N/M3" ;
CON2_8:actual_range = 0.f, 0.f ;
CON2_8:SampledRate = 1 ;
CON2_8:_FillValue = -32767.f ;
float CON2_9(Time) ;
CON2_9:long_name = "PROBE 2/CELL 9 CONCENTRATION (N/M3)" ;
CON2_9:units = "N/M3" ;
CON2_9:actual_range = 0.f, 0.f ;
CON2_9:SampledRate = 1 ;
CON2_9:_FillValue = -32767.f ;
float CON2_10(Time) ;
CON2_10:long_name = "PROBE 2/CELL 10 CONCENTRATION (N/M3)" ;
CON2_10:units = "N/M3" ;
CON2_10:actual_range = 0.f, 0.f ;
CON2_10:SampledRate = 1 ;
CON2_10:_FillValue = -32767.f ;
float CON2_11(Time) ;
CON2_11:long_name = "PROBE 2/CELL 11 CONCENTRATION (N/M3)" ;
CON2_11:units = "N/M3" ;
CON2_11:actual_range = 0.f, 0.f ;
CON2_11:SampledRate = 1 ;
CON2_11:_FillValue = -32767.f ;
float CON2_12(Time) ;
CON2_12:long_name = "PROBE 2/CELL 12 CONCENTRATION (N/M3)" ;
CON2_12:units = "N/M3" ;
CON2_12:actual_range = 0.f, 0.f ;
CON2_12:SampledRate = 1 ;
CON2_12:_FillValue = -32767.f ;
float CON2_13(Time) ;
CON2_13:long_name = "PROBE 2/CELL 13 CONCENTRATION (N/M3)" ;
CON2_13:units = "N/M3" ;
CON2_13:actual_range = 0.f, 0.f ;
CON2_13:SampledRate = 1 ;
CON2_13:_FillValue = -32767.f ;
float CON2_14(Time) ;
CON2_14:long_name = "PROBE 2/CELL 14 CONCENTRATION (N/M3)" ;
CON2_14:units = "N/M3" ;
CON2_14:actual_range = 0.f, 0.f ;
CON2_14:SampledRate = 1 ;
CON2_14:_FillValue = -32767.f ;
float CON2_15(Time) ;
CON2_15:long_name = "PROBE 2/CELL 15 CONCENTRATION (N/M3)" ;
CON2_15:units = "N/M3" ;
CON2_15:actual_range = 0.f, 0.f ;
CON2_15:SampledRate = 1 ;
CON2_15:_FillValue = -32767.f ;
// global attributes:
:institution = "NCAR Research Aviation Facility" ;
:Address = "P.O. Box 3000, Boulder, CO 80307-3000" ;
:creator_url = "http://www.eol.ucar.edu" ;
:Conventions = "NCAR-RAF/nimbus" ;
:ConventionsURL = "http://www.eol.ucar.edu/raf/Software/netCDF.html" ;
:ConventionsVersion = "1.3" ;
:Metadata_Conventions = "Unidata Dataset Discovery v1.0" ;
:standard_name_vocabulary = "CF-1.0" ;
:time_coordinate = "Time" ;
:Phone = "(303) 497-1030" ;
:ProcessorURL = "https://github.com/ncareol/GENPRO" ;
:ProcessorRevision = "8ff1ae2e-dirty" ;
:Categories = "Position,Thermodynamic,Aircraft State,Atmos. State" ;
:geospatial_vertical_positive = "up" ;
:date_created = "2016-08-09T18:38:04 +0000" ;
:Platform = "N307D" ;
:wind_field = "WSPD WDRCTN WI" ;
:time_coverage_start = "1979-05-01T11:11:56 +0000" ;
:time_coverage_end = "1979-05-01T12:50:56 +0000" ;
:TimeInterval = "11:11:56-12:50:56" ;
:FlightDate = "05/01/1979" ;
:geospatial_lat_min = 34.85699f ;
:geospatial_lat_max = 35.688f ;
:latitude_coordinate = "LAT" ;
:geospatial_lon_min = -98.429f ;
:geospatial_lon_max = -95.746f ;
:longitude_coordinate = "LON" ;
:zaxis_coordinate = "HP" ;
:geospatial_vertical_units = "m" ;
:geospatial_vertical_min = 377.f ;
:geospatial_vertical_max = 9472.7f ;
:DESCRIPTION = "743-01 LITTLE SESAME 1 MAY 79 11/06/07" ;
:CYCLE_TIME = 1.f ;
:FlightNumber = "RF01" ;
:ProjectName = "Little SESAME" ;
:converted_from = "G52078" ;
}
SESAME Publications
Data Access
Data Documentation
N304D RAF Data Files for Project SESAME
N304D Sample LRT GENPRO-I header
N304D Sample LRT NetCDF header
N307D RAF Data Files for Project SESAME
Related Links
LRT RAF Data Files for Project: Winter MONEX
LRT RAF Data Files for Project: Winter MONEX
PRODUCTION MASS STORE BITFILE LOG
Project no.: 1979-803 Project name: Winter MONEX
Aircraft: N308D Scientist(s): Joachim Kuettner
Data type: NTI Programmer(s): Jack Martindale
Processor used: GENPRO
Output format: GENPRO-I
HPSS path name: /EOL/1978/wintermonex/aircraft/electra_n308d/NTI/GENPRO-I
HPSS file name: Gxxxxx GxxxxxC
MSS format: TBM COS-blocked copies
------------------------------------------------------------------------------
Date Start End File Sizes (Mbytes)
fltno Gxxxxx mm/dd/yyyy Time Time TBM COS-blocked
------------------------------------------------------------------------------
FF01 G32255 11/17/1978 18:22:09 21:47:20 4.792320 4.599808
FF02A G32256 11/18/1978 16:50:00 17:01:30 10.199040* 1.0014720*
FF02B G32256 11/18/1978 17:03:43 18:40:32
FF02C G32256 11/18/1978 18:42;04 20:43:59
FF02D G32256 11/18/1978 21:00:12 24:35:54
FF03A G32259 11/20/1978 21:54:45 22:07:44 5.038080* 4.874240*
FF03B G32259 11/20/1978 22:08:57 22:56:12
FF03C G32259 11/20/1978 23:07:09 25:43:29
FF04A G32261 11/21/1978 19:53:42 23:44:04 7.004160* 6.791168*
FF04B G32261 11/21/1978 23:44:02 24:56:28
FF05A G32263 11/22/1978 21:55:39 22:51:59 3.317760* 3.149824*
FF05B G32263 11/22/1978 24:45:37 26:09:06
FF05C G32264 11/22/1978 26:00:00 26:29:00 0.860160 0.663552
FF06A G32265 11/25/1978 21:39:43 26:17:23 6.389760 6.230016
FF06B G32266 11/25/1978 26:17:27 26:55:29 1.474560 1.261568
FF07A G32267 11/26/1978 01:48:03 02:05:28 7.127040* 7.028736*
FF07B G32267 11/26/1978 02:10:57 07:06:50
FF08A G32306 01/03/1979 01:19:41 07:22:49 8.232960 8.130560
FF08B G32307 01/03/1979 07:26:08 07:45:25 0.614400 0.442368
FF09 G32308 01/04/1979 01:53:31 07:33:57 7.741440 7.622656
FF10A G32310 01/06/1979 23:18:53 27:09:16 5.283840 5.165056
FF10B G32311 01/06/1979 27:09:14 27:26:10 1.474560* 1.277952*
FF10C G32311 01/06/1979 27:27:05 27:28:19
FF10D G32311 01/06/1979 27:28:56 28:06:31
FF11 G32312 01/07/1979 21:06:37 26:00:30 6.758400 6.586368
FF12A G32314 01/08/1979 02:41:01 03:22:24 4.055040* 3.911680*
FF12B G32314 01/08/1979 03:32:43 05:45:15
FF13A G32315 01/08/1979 19:11:34 23:01:55 9.093120* 8.949760*
FF13B G32315 01/08/1979 23:01:58 25:50:55
FF14A G32317 01/09/1979 16:59:34 19:12:59 4.423680* 4.239360*
FF14B G32317 01/09/1979 19:18:15 20:13:32
RF03A G32274 12/06/1978 02:26:50 02:54:08 7.741440* 7.557120*
RF03B G32274 12/06/1978 03:00:00 08:09:40
RF03C G32276 12/06/1978 08:00:00 08:45:10 3.072000* 2.879488*
RF03D G32276 12/06/1978 08:55:47 10:18:22
RF04A G32277 12/07/1978 03:25:55 03:44:40 10.690560* 10.518528*
RF04B G32277 12/07/1978 03:51:37 07:17:22
RF04C G32277 12/07/1978 07:18:32 08:29:30
RF04D G32277 12/07/1978 08:32:00 11:09:47
RF04E G32277 12/07/1978 11:12:43 11:27:44
RF05 G32280 12/09/1978 01:26:04 05:15:12 5.283840 5.136384
RF06 G32281 12/10/1978 02:03:20 10:16:54 11.182080 11.051008
RF07A G32284 12/11/1978 02:50:28 06:40:50 11.059200* 10.969088*
RF07B G32284 12/11/1978 06:40:48 07:18:17
RF07C G32284 12/11/1978 07:19:39 10:30:25
RF07D G32284 12/11/1978 10:33:38 11:03:47
RF10A G32291 12/16/1978 01:34:58 05:24:07 10.321920* 10.117120*
RF10B G32291 12/16/1978 05:25:21 09:07:48
RF11A G32293 12/17/1978 02:01:21 06:39:40 6.389760 6.234112
RF11B G32294 12/17/1978 06:30:00 09:27:07 4.177920 3.973120
RF12 G32295 12/21/1978 02:12:01 07:01:31 6.635520 6.488064
RF13 G32297 12/24/1978 21:50:09 29:02:15 9.830400 9.674752
RF14A G32299 12/29/1978 00:40:26 07:57:16 10.567680 10.371072
RF14B G32300 12/29/1978 07:30:00 07:57:16 1.843200* 1.728512*
RF14C G32300 12/29/1978 07:57:20 08:46:25
RF15 G32302 12/30/1978 01:21:05 09:00:40 10.444800 10.289152
RF16A G32304 12/31/1978 02:17:42 06:08:05 10.199040 10.113024
RF16B G32305 12/31/1978 06:08:03 09:56:35 5.283840 5.099520
------------------------------------------------------------------------------
* Note: Bitfile size includes multiple flight segments.
W-MONEX Publications
Data Access
W-MONEX Data Documentation
LRT RAF Data Files for Project: Winter MONEX
Sample LRT Header NetCDF Format
Sample HRT Header NetCDF Format
W-MONEX Documents
W-MONEX Photos
W-MONEX Related Links
Sample HRT GENPRO-I header
Sample HRT GENPRO-I header
803-01 MONEX 04DEC78 22/21/48 FIRST TIME ON THIS FILE 26 17 3 THIS FILE I
S ALL OR PART OF TIME PERIOD 22 21 48 TO 29 36 46 DESCRIPTION OF RECORD -- 111 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 665 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 2 CYCLES OF 665 SAMP/CYC = 1330 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 444 60 BIT PACKED WORDS --METHOD OF SCALING-- A BIAS AD(I) WAS ADDED TO EACH SAMPLE
OF EACH PARAMETER TO ELIMINATE ANY NEGATIVE VALUES. THE BIASED SAMPLE WAS THEN MULTIPLIED BY P(I)
TO INSURE THE PROPER NUMBER OF DECIMAL PLACES WERE SAVED. THE PACKED RECORD MAY BE UNPACKED BY RIGH
T JUSTIFYING 20 BITS AT A TIME AND REVERSING THE ABOVE SCALING PROCESS. AS EXAMPLE, S(I)=N/P(I)-AD(I
), WHERE N IS THE 20 BIT SCALED INTEGER, S(I) THE DESIRED UNSCALED PARAMETER, AD(I),P(I) THE CORRESP
ONDING SCALE FACTORS THE ORDER, RATE, PLOT TITLE, PRINT LAB, UNITS, AD AND P SCALE FACTORS OF EACH
PARAMETER FOLLOW
1) 1 PROCESSOR TIME (SECONDS) AFTER MIDNIGHT TIME SEC = (N/ 1.0) - 0.0
2) 1 UNALTERED TAPE TIME (SEC) AFTER MIDNIGHT TPTIME SEC = (N/ 1.0) - 0.0
3) 1 CORRECTED STATIC PRESSURE (MB) PSXC1 MB = (N/ 500.0) - 0.0
4) 1 AMBIENT TEMPERATURE (ROSEMOUNT) (C) ATX1 C = (N/ 1000.0) - 100.0
5) 1 DEWPOINT TEMPERATURE (THERMOELEC) (C) DPXC C = (N/ 1000.0) - 100.0
6) 1 DEWPOINT TEMPERATURE (LYMAN-ALPHA) (C) DPLAC1 C = (N/ 1000.0) - 100.0
7) 1 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
8) 1 ABSOLUTE HUMIDITY (LYMAN-ALPHA) (G/M3) RHOLA1 G/M3 = (N/ 1000.0) - 100.0
9) 1 HORIZONTAL WIND DIRECTION (DEG) WDRCTN DEG = (N/ 1000.0) - 0.0
10) 1 HORIZONTAL WIND SPEED (M/S) WSPD M/S = (N/ 1000.0) - 0.0
11) 1 WIND VECTOR EAST COMPONENT (M/S) UI1 M/S = (N/ 1000.0) - 200.0
12) 1 WIND VECTOR NORTH COMPONENT (M/S) VI1 M/S = (N/ 1000.0) - 200.0
13) 1 WIND VECTOR VERT GUST COMPONENT (M/S) WI1 M/S = (N/ 1000.0) - 100.0
14) 1 WIND VECTOR LNGTDNL COMPONENT (M/S) UX1 M/S = (N/ 1000.0) - 200.0
15) 1 WIND VECTOR LATERAL COMPONENT (M/S) VY1 M/S = (N/ 1000.0) - 200.0
16) 1 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 200.0
17) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
18) 1 NACA PRESSURE ALTITUDE (M) HP M = (N/ 100.0) - 100.0
19) 1 PRESSURE DAMPED INERTIAL ALTITUDE (M) HI31 M = (N/ 100.0) - 100.0
20) 1 GEOMETRIC (RADIO) ALTITUDE (M) HGM M = (N/ 1000.0) - 100.0
21) 1 RAW AIRCRAFT (INS) GROUND SPEED (M/S) GSF1 M/S = (N/ 1000.0) - 0.0
22) 1 AIRCRAFT GROUND SPD EAST COMP (M/S) VEW1 M/S = (N/ 1000.0) - 500.0
23) 1 AIRCRAFT GROUND SPD NORTH COMP (M/S) VNS1 M/S = (N/ 1000.0) - 500.0
24) 1 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP31 M/S = (N/ 1000.0) - 100.0
25) 1 AIRCRAFT C.G. VERT ACCELERATION (M/S2) CGAC1 M/S2 = (N/ 1000.0) - 100.0
26) 1 AIRCRAFT TRUE HEADING (YAW) (DEG) THF1 DEG = (N/ 1000.0) - 0.0
27) 1 AIRCRAFT ROLL ATTITUDE ANGLE (DEG) ROLL1 DEG = (N/ 1000.0) - 100.0
28) 1 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH1 DEG = (N/ 1000.0) - 100.0
29) 1 AIRCRAFT TRUE AIRSPEED (M/S) TASX1 M/S = (N/ 1000.0) - 100.0
30) 1 CORRCTD RADIOMTRC (SFC) TEMP (PRT-5) (C) BPRT5C C = (N/ 1000.0) - 100.0
31) 1 CORRCTD RADIOMTRC (SKY) TEMP (PRT-5) (C) TPRT5C C = (N/ 1000.0) - 100.0
32) 1 DOWNWARD SW/WG-7 IRRADIANCE (WATTS/M2) TPYR1 W/M2 = (N/ 500.0) - 100.0
33) 1 DOWNWARD SW/OG-1 IRRADIANCE (WATTS/M2) TPYR2 W/M2 = (N/ 500.0) - 100.0
34) 1 DOWNWARD SW/RG-8 IRRADIANCE (WATTS/M2) TPYR3 W/M2 = (N/ 500.0) - 100.0
35) 1 UPWARD SW/WG-7 IRRADIANCE (WATTS/M2) BPYR1 W/M2 = (N/ 500.0) - 100.0
36) 1 UPWARD SW/OG-1 IRRADIANCE (WATTS/M2) BPYR2 W/M2 = (N/ 500.0) - 100.0
37) 1 UPWARD SW/RG-8 IRRADIANCE (WATTS/M2) BPYR3 W/M2 = (N/ 500.0) - 100.0
38) 1 CORCTD DOWNWARD IR IRRADIANCE (WATTS/M2) TPYRGC W/M2 = (N/ 1000.0) - 100.0
39) 1 CORCTD UPWARD IR IRRADIANCE (WATTS/M2) BPYRGC W/M2 = (N/ 1000.0) - 100.0
40) 1 CORRCTD J-W LIQUID WATER CONTENT (G/M3) LWCC G/M3 = (N/ 1000.0) - 100.0
41) 1 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB1 C = (N/ 1000.0) - 100.0
42) 1 TOTAL TEMP (FUSELAGE ROSEMOUNT) (C) TTF1 C = (N/ 1000.0) - 100.0
43) 1 DEW/FROST POINT TEMP (L THERMOELEC) (C) DPL C = (N/ 1000.0) - 100.0
44) 1 DEW/FROST POINT TEMP (R THERMOELEC) (C) DPR C = (N/ 1000.0) - 100.0
45) 1 RAW STATIC PRESSURE (WINGTIP) (MB) PSW1 MB = (N/ 500.0) - 0.0
46) 1 RAW DYNAMIC PRESSURE (WINGTIP) (MB) QCW1 MB = (N/ 1000.0) - 100.0
47) 1 RAW STATIC PRESSURE (BOOM) (MB) PSB1 MB = (N/ 500.0) - 0.0
48) 1 RAW DYNAMIC PRESSURE (BOOM) (MB) QCB1 MB = (N/ 1000.0) - 100.0
49) 1 DISTANCE EAST OF START (KM) DEI KM = (N/ 100.0) - 5000.0
50) 1 DISTANCE NORTH OF START (KM) DNI KM = (N/ 100.0) - 5000.0
51) 1 LTN-51 ARINC TIME LAG (SEC) TMLAG SEC = (N/ 1000.0) - 100.0
52) 1 INS WANDER ANGLE (DEG) ALPHA DEG = (N/ 1000.0) - 100.0
53) 1 AIRCRAFT TRUE HEADING (ARINC) (DEG) THI DEG = (N/ 1000.0) - 100.0
54) 1 RAW DOWNWARD IR IRRADIANCE (WATTS/M2) TPYRG W/M2 = (N/ 1000.0) - 500.0
55) 1 RAW UPWARD IR IRRADIANCE (WATTS/M2) BPYRG W/M2 = (N/ 1000.0) - 500.0
56) 1 TOP PYRGEOMETER DOME TEMP (C) TPGDT C = (N/ 1000.0) - 100.0
57) 1 TOP PYRGEOMETER SINK TEMP (C) TPGST C = (N/ 1000.0) - 100.0
58) 1 BOTTOM PYRGEOMETER DOME TEMP (C) BPGDT C = (N/ 1000.0) - 100.0
59) 1 BOTTOM PYRGEOMETER SINK TEMP (C) BPGST C = (N/ 1000.0) - 100.0
60) 1 BOTTOM PRT-5 IRTRAN WINDOW TEMP (C) BP5WT C = (N/ 1000.0) - 100.0
61) 1 BTM RAW RADIOMTRC (SFC) TEMP (PRT-5) (C) BPRT5 C = (N/ 1000.0) - 100.0
62) 1 TOP PRT-5 IRTRAN WINDOW TEMPERATURE (C) TP5WT C = (N/ 1000.0) - 100.0
63) 1 TOP RAW RADIOMTRC (SKY) TEMP (PRT-5) (C) TPRT5 C = (N/ 1000.0) - 100.0
64) 1 RAW J-W LIQUID WATER CONTENT (G/M3) LWC G/M3 = (N/ 1000.0) - 100.0
65) 1 16MM CAMERA FRAME COUNT CAMFC = (N/ 1.0) - 0.0
66) 1 EVENT MARKER WORD (16 BITS) EVMRKS = (N/ 1.0) - 0.0
67) 1 INS/KNOLLENBERG UPDATE FLAGS IKFLG = (N/ 1.0) - 0.0
68) 1 PRESSURE CABIN (MB) PCAB MB = (N/ 500.0) - 0.0
69) 20 AMBIENT TEMPERATURE (FAST RESPONSE) (C) ATKP C = (N/ 1000.0) - 100.0
70) 20 AMBIENT TEMP (COMPNSTD BOOM ROSMNT) (C) ATBC C = (N/ 1000.0) - 100.0
71) 20 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 100.0
72) 20 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0
73) 20 WIND VECTOR VERT GUST COMPONENT(HR)(M/S) WI M/S = (N/ 1000.0) - 200.0
74) 20 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0
75) 20 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0
76) 20 ABSOLUTE HUMIDITY (LYMN-ALPHA HR) (G/M3) RHOLA G/M3 = (N/ 1000.0) - 100.0
77) 20 RAW LYMAN-ALPHA HYGROMETER OUTPUT (VDC) LAV VDC = (N/ 1000.0) - 100.0
78) 20 TOTAL TEMPERATURE (FAST RESPONSE) (C) TTKP C = (N/ 1000.0) - 100.0
79) 20 TOTAL TEMP (COMPENSATED BOOM ROSMNT) (C) TTBC C = (N/ 1000.0) - 100.0
80) 20 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB C = (N/ 1000.0) - 100.0
81) 20 RAW DYNAMIC PRESSURE (GUST PROBE) (MB) QCG MB = (N/ 1000.0) - 100.0
82) 20 ATTACK ANGLE (ROTATING VANE) (DEG) AROT DEG = (N/ 1000.0) - 100.0
83) 20 ATTACK ANGLE (FIXED VANE) (DEG) AFIX DEG = (N/ 1000.0) - 100.0
84) 20 SIDESLIP ANGLE (ROTATING VANE) (DEG) BROT DEG = (N/ 1000.0) - 100.0
85) 20 SIDESLIP ANGLE (FIXED VANE) (DEG) BFIX DEG = (N/ 1000.0) - 100.0
86) 20 GUST PROBE TIP VERT ACCELERATION (M/S2) VAC M/S2 = (N/ 1000.0) - 100.0
87) 20 GUST PROBE TIP LATERAL ACCEL. (M/S2) LAC M/S2 = (N/ 1000.0) - 100.0
88) 20 AIRCRAFT C.G. VERT ACCEL. (HR) (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
89) 20 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 100.0) - 5000.0
90) 20 AIRCRAFT ROLL ATTITUDE ANGLE (HR) (DEG) ROLL DEG = (N/ 1000.0) - 100.0
91) 20 AIRCRAFT PITCH ATTITUDE ANGLE (HR) (DEG) PITCH DEG = (N/ 1000.0) - 100.0
92) 20 AIRCRAFT TRUE HEADING (YAW) (HR) (DEG) THF DEG = (N/ 1000.0) - 100.0
93) 20 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
94) 20 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
95) 16 P M S OAP-200X ACCUMS. (ID + 15 CELLS) OAP200X ACCUM = (N/ 1.0) - 0.0
96) 16 P M S OAP-200Y ACCUMS. (ID + 15 CELLS) OAP200Y ACCUM = (N/ 1.0) - 0.0
97) 16 P M S ASAS ACCUMULATIONS (ID + 15 CELLS) ASAS ACCUM = (N/ 1.0) - 0.0
98) 16 P M S FSSP ACCUMULATIONS (ID + 15 CELLS) FSSP ACCUM = (N/ 1.0) - 0.0
99) 1 TOP UV RADIOMETER (290-315NM) (VDC) TUVR3 VDC = (N/ 1000.0) - 100.0
100) 1 TOP UV RADIOMETER (290-380NM) (VDC) TUVR4 VDC = (N/ 1000.0) - 100.0
101) 1 BOTTOM UV RADIOMETER (290-315NM) (VDC) BUVR3 VDC = (N/ 1000.0) - 100.0
102) 1 BOTTOM UV RADIOMETER (290-380NM) (VDC) BUVR4 VDC = (N/ 1000.0) - 100.0
103) 1 ACTINOMETER PRESSURE (VDC) PACTN VDC = (N/ 1000.0) - 100.0
104) 1 NCAR DASIBI OZONE OUTPUT (DELANY) (VDC) NDO3 VDC = (N/ 1000.0) - 100.0
105) 1 NCAR CSI ETHYLENE OZONE OUTPUT (VDC) NEO3 VDC = (N/ 1000.0) - 100.0
106) 1 NOX OUTPUT (DICKERSON) (VDC) NOXDN VDC = (N/ 1000.0) - 100.0
107) 1 NOX OUTPUT (DELANY) (COUNTS) NOXDY COUNTS = (N/ 1.0) - 0.0
108) 1 NOX PRESSURE (DELANY) (VDC) PRNOX VDC = (N/ 1000.0) - 100.0
109) 1 NOX FLOW SIGNAL (DELANY) (VDC) FLNOX VDC = (N/ 1000.0) - 100.0
110) 1 HOT WIRE OUTPUT (LA RUE) (VDC) HWOLR VDC = (N/ 1000.0) - 100.0
111) 1 FIXED ANGLE NEPHELOMETER OUTPUT (VDC) FANEPH VDC = (N/ 1000.0) - 100.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
803-01 MONEX 04DEC78 22/21/48
THIS FILE IS ALL OR PART OF THE TIME PERIOD 22 21 48 TO 29 36 46
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
676 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
562432 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 13300 BITS PER LOGICAL DATA RECORD
2 LOGICAL DATA RECORDS PER PHYSICAL RECORD
26600 BITS PER PHYSICAL DATA RECORD
W-MONEX Publications
Data Access
W-MONEX Data Documentation
LRT RAF Data Files for Project: Winter MONEX
Sample LRT Header NetCDF Format
Sample HRT Header NetCDF Format
W-MONEX Documents
W-MONEX Photos
W-MONEX Related Links
Sample LRT GENPRO-I header
Sample LRT GENPRO-I header
803-03 MONEX 6DEC78 02/26/50 FIRST TIME ON THIS FILE 2 26 49 THIS FILE I
S ALL OR PART OF TIME PERIOD 2 26 50 TO 10 18 25 DESCRIPTION OF RECORD -- 88 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 148 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 10 CYCLES OF 148 SAMP/CYC = 1480 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 494 60 BIT PACKED WORDS --METHOD OF SCALING-- A BIAS AD(I) WAS ADDED TO EACH SAMPLE
OF EACH PARAMETER TO ELIMINATE ANY NEGATIVE VALUES. THE BIASED SAMPLE WAS THEN MULTIPLIED BY P(I)
TO INSURE THE PROPER NUMBER OF DECIMAL PLACES WERE SAVED. THE PACKED RECORD MAY BE UNPACKED BY RIGH
T JUSTIFYING 20 BITS AT A TIME AND REVERSING THE ABOVE SCALING PROCESS. AS EXAMPLE, S(I)=N/P(I)-AD(I
), WHERE N IS THE 20 BIT SCALED INTEGER, S(I) THE DESIRED UNSCALED PARAMETER, AD(I),P(I) THE CORRESP
ONDING SCALE FACTORS THE ORDER, RATE, PLOT TITLE, PRINT LAB, UNITS, AD AND P SCALE FACTORS OF EACH
PARAMETER FOLLOW
1) 1 PROCESSOR TIME (SECONDS) AFTER MIDNIGHT TIME SEC = (N/ 1.0) - 0.0
2) 1 UNALTERED TAPE TIME (SEC) AFTER MIDNIGHT TPTIME SEC = (N/ 1.0) - 0.0
3) 1 LTN-51 ARINC TIME LAG (SEC) TMLAG SEC = (N/ 1000.0) - 100.0
4) 1 INS/KNOLLENBERG UPDATE FLAGS IKFLG = (N/ 1.0) - 0.0
5) 1 FIXED ZERO INPUT (A/D CHECK) (VDC) FZV VDC = (N/ 1000.0) - 100.0
6) 1 D/A OUTPUT (CALIBRATION CHECK) (VDC) D2AOUT VDC = (N/ 1000.0) - 100.0
7) 1 EVENT MARKER WORD (16 BITS) EVMRKS = (N/ 1.0) - 0.0
8) 1 16MM CAMERA FRAME COUNT CAMFC = (N/ 1.0) - 0.0
9) 1 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 200.0
10) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
11) 1 AIRCRAFT TRUE HEADING (ARINC) (DEG) THI DEG = (N/ 1000.0) - 100.0
12) 1 INS WANDER ANGLE (DEG) ALPHA DEG = (N/ 1000.0) - 100.0
13) 1 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
14) 1 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
15) 1 RAW AIRCRAFT (INS) GROUND SPEED (M/S) GSF1 M/S = (N/ 1000.0) - 0.0
16) 1 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 100.0) - 5000.0
17) 1 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH DEG = (N/ 1000.0) - 100.0
18) 1 AIRCRAFT ROLL ATTITUDE ANGLE (HR) (DEG) ROLL DEG = (N/ 1000.0) - 100.0
19) 1 AIRCRAFT TRUE HEADING (YAW) (HR) (DEG) THF DEG = (N/ 1000.0) - 0.0
20) 1 RAW DYNAMIC PRESSURE (BOOM) (MB) QCB1 MB = (N/ 1000.0) - 100.0
21) 1 RAW DYNAMIC PRESSURE (WINGTIP) (MB) QCW1 MB = (N/ 1000.0) - 100.0
22) 1 RAW STATIC PRESSURE (BOOM) (MB) PSB1 MB = (N/ 500.0) - 0.0
23) 1 RAW STATIC PRESSURE (WINGTIP) (MB) PSW1 MB = (N/ 500.0) - 0.0
24) 1 CORRECTED STATIC PRESSURE (MB) PSXC1 MB = (N/ 500.0) - 0.0
25) 1 NACA PRESSURE ALTITUDE (M) HP M = (N/ 100.0) - 100.0
26) 1 GEOMETRIC (RADIO) ALTITUDE (M) HGM M = (N/ 1000.0) - 100.0
27) 1 CABIN PRESSURE (MB) PCAB MB = (N/ 500.0) - 0.0
28) 1 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB1 C = (N/ 1000.0) - 100.0
29) 1 TOTAL TEMP (FUSELAGE ROSEMOUNT) (C) TTF1 C = (N/ 1000.0) - 100.0
30) 1 AMBIENT TEMPERATURE (ROSEMOUNT) (C) ATX1 C = (N/ 1000.0) - 100.0
31) 1 AIRCRAFT TRUE AIRSPEED (M/S) TASX1 M/S = (N/ 1000.0) - 100.0
32) 1 DEW/FROST POINT TEMP (L THERMOELEC) (C) DPL C = (N/ 1000.0) - 100.0
33) 1 DEW/FROST POINT TEMP (R THERMOELEC) (C) DPR C = (N/ 1000.0) - 100.0
34) 1 DEWPOINT TEMPERATURE (THERMOELEC) (C) DPXC C = (N/ 1000.0) - 100.0
35) 1 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
36) 1 RAW LYMAN-ALPHA HYGROMETER OUTPUT (VDC) LAV VDC = (N/ 1000.0) - 100.0
37) 1 RAW J-W LIQUID WATER CONTENT (G/M3) LWC G/M3 = (N/ 1000.0) - 100.0
38) 1 CORRCTD J-W LIQUID WATER CONTENT (G/M3) LWCC G/M3 = (N/ 1000.0) - 100.0
39) 1 DOWNWARD SW/WG-7 IRRADIANCE (WATTS/M2) TPYR1 W/M2 = (N/ 500.0) - 100.0
40) 1 DOWNWARD SW/OG-1 IRRADIANCE (WATTS/M2) TPYR2 W/M2 = (N/ 500.0) - 100.0
41) 1 DOWNWARD SW/RG-8 IRRADIANCE (WATTS/M2) TPYR3 W/M2 = (N/ 500.0) - 100.0
42) 1 RAW DOWNWARD IR IRRADIANCE (WATTS/M2) TPYRG W/M2 = (N/ 1000.0) - 100.0
43) 1 UPPER PYRGEOMETER DOME TEMP (C) TPGDT C = (N/ 1000.0) - 100.0
44) 1 UPPER PYRGEOMETER SINK TEMP (C) TPGST C = (N/ 1000.0) - 100.0
45) 1 UPWARD SW/WG-7 IRRADIANCE (WATTS/M2) BPYR1 W/M2 = (N/ 500.0) - 100.0
46) 1 UPWARD SW/OG-1 IRRADIANCE (WATTS/M2) BPYR2 W/M2 = (N/ 500.0) - 100.0
47) 1 UPWARD SW/RG-8 IRRADIANCE (WATTS/M2) BPYR3 W/M2 = (N/ 500.0) - 100.0
48) 1 RAW UPWARD IR IRRADIANCE (WATTS/M2) BPYRG W/M2 = (N/ 1000.0) - 100.0
49) 1 LOWER PYRGEOMETER DOME TEMP (C) BPGDT C = (N/ 1000.0) - 100.0
50) 1 LOWER PYRGEOMETER SINK TEMP (C) BPGST C = (N/ 500.0) - 100.0
51) 1 CORCTD DOWNWARD IR IRRADIANCE (WATTS/M2) TPYRGC W/M2 = (N/ 500.0) - 100.0
52) 1 CORCTD UPWARD IR IRRADIANCE (WATTS/M2) BPYRGC W/M2 = (N/ 500.0) - 100.0
53) 1 BOTTOM PRT-5 IRTRAN WINDOW TEMP (C) BP5WT C = (N/ 1000.0) - 100.0
54) 1 BTM RAW RADIOMTRC (SFC) TEMP (PRT-5) (C) BPRT5 C = (N/ 1000.0) - 100.0
55) 1 CORRCTD RADIOMTRC (SFC) TEMP (PRT-5) (C) BPRT5C C = (N/ 1000.0) - 100.0
56) 1 TOP PRT-5 IRTRAN WINDOW TEMPERATURE (C) TP5WT C = (N/ 1000.0) - 100.0
57) 1 TOP RAW RADIOMTRC (SKY) TEMP (PRT-5) (C) TPRT5 C = (N/ 1000.0) - 100.0
58) 1 CORRCTD RADIOMTRC (SKY) TEMP (PRT-5) (C) TPRT5C C = (N/ 1000.0) - 100.0
59) 1 AIRCRAFT C.G. VERT ACCELERATION (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
60) 1 HORIZONTAL WIND DIRECTION (DEG) WDRCTN DEG = (N/ 1000.0) - 0.0
61) 1 HORIZONTAL WIND SPEED (M/S) WSPD M/S = (N/ 1000.0) - 0.0
62) 1 WIND VECTOR EAST COMPONENT (M/S) UI1 M/S = (N/ 1000.0) - 200.0
63) 1 WIND VECTOR NORTH COMPONENT (M/S) VI1 M/S = (N/ 1000.0) - 200.0
64) 1 WIND VECTOR LNGTDNL COMPONENT (M/S) UX1 M/S = (N/ 1000.0) - 200.0
65) 1 WIND VECTOR LATERAL COMPONENT (M/S) VY1 M/S = (N/ 1000.0) - 200.0
66) 1 AIRCRAFT GROUND SPD EAST COMP (M/S) VEW1 M/S = (N/ 1000.0) - 500.0
67) 1 AIRCRAFT GROUND SPD NORTH COMP (M/S) VNS1 M/S = (N/ 1000.0) - 500.0
68) 1 DISTANCE EAST OF START (KM) DEI KM = (N/ 100.0) - 5000.0
69) 1 DISTANCE NORTH OF START (KM) DNI KM = (N/ 100.0) - 5000.0
70) 1 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP31 M/S = (N/ 1000.0) - 100.0
71) 1 PRESSURE DAMPED INERTIAL ALTITUDE (M) HI31 M = (N/ 10.0) - 500.0
72) 1 TOP UV RADIOMETER (290-315NM) (VDC) TUVR3 VDC = (N/ 1000.0) - 100.0
73) 1 TOP UV RADIOMETER (290-380NM) (VDC) TUVR4 VDC = (N/ 1000.0) - 100.0
74) 1 BOTTOM UV RADIOMETER (290-315NM) (VDC) BUVR3 VDC = (N/ 1000.0) - 100.0
75) 1 BOTTOM UV RADIOMETER (290-380NM) (VDC) BUVR4 VDC = (N/ 1000.0) - 100.0
76) 1 ACTINOMETER PRESSURE (VDC) PACTN VDC = (N/ 1000.0) - 100.0
77) 1 NCAR DASIBI OZONE OUTPUT (DELANY) (VDC) NDO3 VDC = (N/ 1000.0) - 100.0
78) 1 NOX PRESSURE (DELANY) (VDC) PRNOX VDC = (N/ 1000.0) - 100.0
79) 1 NOX OUTPUT (DICKERSON) (VDC) NOXDN VDC = (N/ 1000.0) - 100.0
80) 1 NCAR CSI ETHYLENE OZONE OUTPUT (VDC) NEO3 VDC = (N/ 1000.0) - 100.0
81) 1 FIXED ANGLE NEPHELOMETER OUTPUT (VDC) FANEPH VDC = (N/ 1000.0) - 100.0
82) 1 NOX FLOW SIGNAL (DELANY) (VDC) FLNOX VDC = (N/ 1000.0) - 100.0
83) 1 HOT WIRE OUTPUT (LA RUE) (VDC) HWOLR VDC = (N/ 1000.0) - 100.0
84) 1 NOX OUTPUT (DELANY) (COUNTS) NOXDY COUNTS = (N/ 1.0) - 0.0
85) 16 P M S OAP-200X ACCUMS. (ID + 15 CELLS) OAP200X ACCUM = (N/ 1.0) - 0.0
86) 16 P M S OAP-200Y ACCUMS. (ID + 15 CELLS) OAP200Y ACCUM = (N/ 1.0) - 0.0
87) 16 P M S ASAS ACCUMULATIONS (ID + 15 CELLS) ASAS ACCUM = (N/ 1.0) - 0.0
88) 16 P M S FSSP ACCUMULATIONS (ID + 15 CELLS) FSSP ACCUM = (N/ 1.0) - 0.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
803-03 MONEX 6DEC78 02/26/50
THIS FILE IS ALL OR PART OF THE TIME PERIOD 2 26 50 TO 10 18 25
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
159 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
132288 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 2960 BITS PER LOGICAL DATA RECORD
10 LOGICAL DATA RECORDS PER PHYSICAL RECORD
29600 BITS PER PHYSICAL DATA RECORD
W-MONEX Publications
Data Access
W-MONEX Data Documentation
LRT RAF Data Files for Project: Winter MONEX
Sample LRT Header NetCDF Format
Sample HRT Header NetCDF Format
W-MONEX Documents
W-MONEX Photos
W-MONEX Related Links