Sample HRT GENPRO-I header
866-01 STREX 15NOV80 18 55 58 FIRST TIME ON THIS FILE 18 56 7 THIS FILE I
S ALL OR PART OF TIME PERIOD 18 55 58 TO 26 45 40 DESCRIPTION OF RECORD -- 95 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 672 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 2 CYCLES OF 672 SAMP/CYC = 1344 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 448 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(BOOM)(LR)(MB) PSBC1 MB = (N/ 500.0) - 0.0
4) 1 AMBIENT TEMPERATURE (BOOM)(LR) (C) ATB1 C = (N/ 1000.0) - 100.0
5) 1 POTENTIAL TEMPERATURE (LR) (K) THETA1 K = (N/ 1000.0) - 100.0
6) 1 DEWPOINT TEMPERATURE (THERM.)(EG&G)(C) DPRTC C = (N/ 1000.0) - 100.0
7) 1 DEWPOINT TEMP.(GENERAL EASTERN)(C) DPRBC C = (N/ 1000.0) - 100.0
8) 1 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
9) 1 HORIZONTAL WIND DIRECTION (LR)(DEG) WDRCTN1 DEG = (N/ 1000.0) - 0.0
10) 1 HORIZONTAL WIND SPEED (LR)(M/S) WSPD1 M/S = (N/ 1000.0) - 0.0
11) 1 WIND VECTOR EAST COMPONENT (LR)(M/S) UI1 M/S = (N/ 1000.0) - 200.0
12) 1 WIND VECTOR NORTH COMPONENT(LR) (M/S) VI1 M/S = (N/ 1000.0) - 200.0
13) 1 WIND VECTOR VERTICAL GUST COMP(LR)(M/S) WI1 M/S = (N/ 1000.0) - 100.0
14) 1 WIND VECTOR LNGTDNL COMP.(LR) (M/S) UX1 M/S = (N/ 1000.0) - 200.0
15) 1 WIND VECTOR LATERAL COMP.(LR) (M/S) VY1 M/S = (N/ 1000.0) - 200.0
16) 1 NACA PRESSURE ALTITUDE (LR) (M) HP1 M = (N/ 10.0) - 500.0
17) 1 PRESSURE-DAMPED INERTIAL ALTITUDE(LR)(M) HI31 M = (N/ 10.0) - 500.0
18) 1 COARSE ALTITUDE SYNCHRO (DEG) CHGME DEG = (N/ 1000.0) - 100.0
19) 1 FINE ALTITUDE SYNCHRO (DEG) HGME DEG = (N/ 1000.0) - 100.0
20) 1 ALTITUDE (M) (APN-159) ALT M = (N/ 10.0) - 500.0
21) 1 RAW INS GROUND SPD EAST COMP.(LR)(M/S) VEW1 M = (N/ 1000.0) - 500.0
22) 1 RAW INS GROUND SPD NORTH COMP.(LR)(M/S) VNS1 M = (N/ 1000.0) - 500.0
23) 1 DAMPED AIRCRAFT VERT VELOCITY(LR)(M/S) WP31 M/S = (N/ 1000.0) - 100.0
24) 1 AIRCRAFT C.G. ACCELERATION (LR)(M/S2) CGAC1 M/S2 = (N/ 1000.0) - 100.0
25) 1 AIRCRAFT TRUE HEADING (YAW)(LR) (DEG) THF1 DEG = (N/ 1000.0) - 0.0
26) 1 AIRCRAFT ROLL ATTITUDE ANGLE(LR) (DEG) ROLL1 DEG = (N/ 1000.0) - 100.0
27) 1 AIRCRAFT PITCH ATTITUDE ANGLE(LR)(DEG) PITCH1 DEG = (N/ 1000.0) - 100.0
28) 1 AIRCRAFT TRUE AIRSPEED (WING) (M/S) TASW1 M/S = (N/ 1000.0) - 100.0
29) 1 RAW IR SURF TEMP 9.5-11.5 MIC(PRT-5)(C) PRT-5 C = (N/ 1000.0) - 100.0
30) 1 RAW IR SKY TEMP 9.5-11.5 MIC(PRT-6)(C) PRT-6 C = (N/ 1000.0) - 100.0
31) 1 RAW BOTTOM PYRANOMETER OUTPUT (WG-7) (WA BPYR1 WATTS/M2 = (N/ 500.0) - 100.0
32) 1 RAW BOTTOM PYRANOMETER OUTPUT (OG-1) (WA BPYR2 WATTS/M2 = (N/ 500.0) - 100.0
33) 1 RAW BOTTOM PYRANOMETER OUTPUT (RG-8) (WA BPYR3 WATTS/M2 = (N/ 500.0) - 100.0
34) 1 RAW TOP PYRANOMETER OUTPUT (WG-7) (WAT TPYR1 WATTS/M2 = (N/ 500.0) - 100.0
35) 1 RAW TOP PYRANOMETER OUTPUT (RG-8) (WAT TPYR2 WATTS/M2 = (N/ 500.0) - 100.0
36) 1 RAW TOP PYRANOMETER OUTPUT (RG-8) (WAT TPYR3 WATTS/M2 = (N/ 500.0) - 100.0
37) 1 CORRECTED BOTTOM PYRGEOMETER OUTPUT (WAT BPYRGC WATTS/M2 = (N/ 1000.0) - 100.0
38) 1 CORRECTED TOP PYRGEOMETER OUTPUT (WATT TPYRGC WATTS/M2 = (N/ 1000.0) - 100.0
39) 1 CORRCTD J-W LIQUID WATER CONTENT (G/M3) LWCC G/M3 = (N/ 1000.0) - 100.0
40) 1 TOTAL TEMPERATURE(BOOM ROSMT)(LR)(C) TTB1 C = (N/ 1000.0) - 100.0
41) 1 DEW/FROSTPOINT TEMP (EG&G) (C) DPRT C = (N/ 1000.0) - 100.0
42) 1 DEW/FROSTPOINT TEMP(GENERAL EASTERN)(C) DPRB C = (N/ 1000.0) - 100.0
43) 1 RAW DYNAMIC PRESSURE (WING)(LR)(MB) PSW1 MB = (N/ 500.0) - 0.0
44) 1 RAW DYNAMIC PRESSURE(WING)(LR)(MB) QCW1 MB = (N/ 1000.0) - 100.0
45) 1 RAW STATIC PRESSURE (BOOM)(LR) (MB) PSB1 MB = (N/ 500.0) - 0.0
46) 1 RAW DYNAMIC PRESSURE (LR) (BOOM) (MB) QCB1 MB = (N/ 1000.0) - 100.0
47) 1 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 200.0
48) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
49) 1 INS WANDER ANGLE (DEG) (LR) ALPHA1 DEG = (N/ 1000.0) - 100.0
50) 1 AIRCRAFT TRUE HEADING (LR)(ARINC)(DEG) THI1 DEG = (N/ 1000.0) - 100.0
51) 1 RAW BOTTOM PYRGEOMETER OUTPUT (WATTS/M2) BPYRG WATTS/M2 = (N/ 100.0) - 1000.0
52) 1 RAW TOP PYRGEOMETER OUTPUT (WATTS/M2) TPYRG WATTS/M2 = (N/ 100.0) - 1000.0
53) 1 BOTTOM PYRGEOMETER DOME TEMPERATURE (C) BPGDT C = (N/ 1000.0) - 100.0
54) 1 BOTTOM PYRGEOMETER SINK TEMPERATURE (C) BPGST C = (N/ 1000.0) - 100.0
55) 1 TOP PYRGEOMETER DOME TEMPERATURE (C) TPGDT C = (N/ 1000.0) - 100.0
56) 1 TOP PYRGEOMETER SINK TEMPERATURE (C) TPGST C = (N/ 1000.0) - 100.0
57) 1 RAW J-W LIQUID WATER CONTENT (G/M3) LWC G/M3 = (N/ 1000.0) - 100.0
58) 20 AMBIENT TEMP. (COMP. BOOM) (C) ATBC C = (N/ 1000.0) - 100.0
59) 20 POTENTIAL TEMPERATURE (K) THETA K = (N/ 1000.0) - 100.0
60) 20 AMBIENT TEMPERATURE (DEICED ROSEMT)(C) ATFH C = (N/ 1000.0) - 100.0
61) 20 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 200.0
62) 20 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0
63) 20 WIND VECTOR VERTICAL GUST COMP. (M/S) WI M/S = (N/ 1000.0) - 100.0
64) 20 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0
65) 20 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0
66) 20 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP3 M/S = (N/ 1000.0) - 100.0
67) 20 LYMAN-ALPHA (VDC) VLA VDC = (N/ 1000.0) - 100.0
68) 20 TOTAL TEMP. (DEICED ROSEMOUNT) (C) TTFH C = (N/ 1000.0) - 100.0
69) 20 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB C = (N/ 1000.0) - 100.0
70) 20 TOTAL TEMP. (COMP. BOOM ROSEMOUNT) (C) TTBC C = (N/ 1000.0) - 100.0
71) 20 RAW DYNAMIC PRESSURE (GUST PROBE) (MB) QCG MB = (N/ 1000.0) - 100.0
72) 20 ATTACK ANGLE (FIXED VANE LEFT SIDE) AFIXL DEG = (N/ 1000.0) - 100.0
73) 20 ATTACK ANGLE (FIXED VANE RIGHT SIDE) AFIXR DEG = (N/ 1000.0) - 100.0
74) 20 SIDE SLIP ANGLE (FIXED VANE TOP) (DEG) BFIXT DEG = (N/ 1000.0) - 100.0
75) 20 SIDE SLIP ANGLE (FIXED VANE BOTTOM) BFIXB DEG = (N/ 1000.0) - 100.0
76) 20 AIRCRAFT C.G. ACCELERATION (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
77) 20 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 100.0) - 5000.0
78) 20 AIRCRAFT ROLL ATTITUDE ANGLE (DEG) ROLL DEG = (N/ 1000.0) - 100.0
79) 20 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH DEG = (N/ 1000.0) - 100.0
80) 20 AIRCRAFT TRUE HEADING (YAW) (DEG) THF DEG = (N/ 1000.0) - 100.0
81) 20 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
82) 20 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
83) 20 AIRCRAFT GROUND SPEED (M/S) GSF M/S = (N/ 1000.0) - 100.0
84) 20 AIRCRAFT TRUE AIRSPEED (GUST PROBE)(M/S) TASGB M/S = (N/ 1000.0) - 100.0
85) 20 FAST OZONE (25 HZ) (VDC) FO3 VDC = (N/ 1000.0) - 100.0
86) 16 PMS PROBE 1 FSSP (ID AND ACC.) PMSPB1 FSSP = (N/ 1.0) - 0.0
87) 16 PMS PROBE 2 200X (ID AND ACC.) PMSPB2 200X = (N/ 1.0) - 0.0
88) 16 PMS PROBE 3 PMS3 (ID AND ACC.) PMSPB3 PMS3 = (N/ 1.0) - 0.0
89) 1 EVENT MARKER WORD EVMRKS = (N/ 1000.0) - 100.0
90) 1 MEAN OZONE (PPM) 03M PPM = (N/ 1000.0) - 100.0
91) 1 03 PMT TEMPERATURE (C) 03PMT (C) = (N/ 1000.0) - 100.0
92) 1 03 CHAMBER TEMPERATURE (5 HZ) (C) 03RCT (C) = (N/ 1000.0) - 100.0
93) 1 03 CHAMBER PRESSURE (5 HZ) (TORR) 03RCP (TORR) = (N/ 1000.0) - 100.0
94) 1 COOLER TEMPERATURE (HS1) (VDC) CHS1 (VDC) = (N/ 1000.0) - 100.0
95) 1 BOOM STATIC PRESSURE TEMPERATURE (C) TPSB (C) = (N/ 1000.0) - 100.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
1 866-01 STREX 15NOV80 18 55 58
THIS FILE IS ALL OR PART OF THE TIME PERIOD 18 55 58 TO 26 45 40
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
683 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
568256 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 13440 BITS PER LOGICAL DATA RECORD
2 LOGICAL DATA RECORDS PER PHYSICAL RECORD
26880 BITS PER PHYSICAL DATA RECORD
PROJECT FLIGHT DATE
PROJECT FLIGHT TIME 18 56 7
MACHINE = 7600
95 PARAMETERS WERE SAVED AT THEIR RESPECTIVE RATES
672 SAMPLES WERE SCALED INTO 20 BIT INTEGER WORDS.
STREX Publications
Data Access
STREX Documentation
RAF Data Files for Project: STREX (Storm Transfer andResponse EXperiment)
STREX Documents
- Operations Plan, Storm Transfer and Response Experiment (STREX) International STREX Office, 27 October 1980.
- Workshop Summary on First Scientific Results, STREX Data Center, September 1981.
- Field Phase Report, Storm Transfer and Response Experiment (STREX), STREX Data Center, May 1981.
- Meteorological Atlas, Storm Transfer and Response Experiment (STREX), STREX Data Center, 30 June 1981.