```  805-03 ALPEX  HRT 06MAR1982                       FIRST TIME ON THIS FILE  9 49 54       THIS FILE I
S ALL OR PART OF TIME PERIOD  9 49 45 TO 17  4  0  DESCRIPTION OF RECORD --  96 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  594 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE  2 CYCLES OF 594 SAMP/CYC = 1188 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 396 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)(MB)        PSBC1      MB     = (N/  500.0) -    0.0
4)   1     AMBIENT TEMP.2(BOOM ROSEM.ECTRON)(LR)(C)    ATB2L      C     = (N/ 1000.0) -  100.0
5)   1     AMBIENT TEMP (BOOM)(LR) (ATB1)      (C)     ATB1       C     = (N/ 1000.0) -  100.0
6)   1     AMBIENT TEMPERATURE (DEICED ROSEMT)(C)       ATFH      C     = (N/ 1000.0) -  100.0
7)   1     DEWPOINT TEMPERATURE (TOP)(EG&G)(C)        DPRTC     C       = (N/ 1000.0) -  100.0
8)   1     DEWPOINT TEMP. (BOT EG&G)    (C)           DPRBC     C       = (N/ 1000.0) -  100.0
9)   1     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)      RHOTD     G/M3    = (N/ 1000.0) -  100.0
10)   1     HORIZONTAL WIND DIRECTION (LR)    (DEG)  WDRCTN1         DEG = (N/ 1000.0) -    0.0
11)   1     HORIZONTAL WIND SPEED (LR)        (M/S)   WSPD1          M/S = (N/ 1000.0) -    0.0
12)   1     WIND VECTOR EAST COMPONENT (LR)   (M/S)      UI1        M/S  = (N/ 1000.0) -  200.0
13)   1     WIND VECTOR NORTH COMPONENT (LR)  (M/S)      VI1        M/S  = (N/ 1000.0) -  200.0
14)   1     WIND VECTOR VERTICAL COMP(LR)(M/S)           WI1        M/S  = (N/ 1000.0) -  100.0
15)   1     WIND VECTOR LNGTDNL  COMP.(LR)    (M/S)    UX1     M/S       = (N/ 1000.0) -  200.0
16)   1     WIND VECTOR LATERAL  COMP.(LR)1   (M/S)    VY1     M/S       = (N/ 1000.0) -  200.0
17)   1     NACA PRESSURE ALTITUDE          (M)         HP1       M      = (N/   10.0) -  500.0
18)   1     PRESSURE-DAMPED INERTIAL ALT    (M)         HI3L       M     = (N/   10.0) -  500.0
19)   1     GEOMETRIC (RADIO) ALT   (M)                 HGM        M     = (N/ 1000.0) -  100.0
20)   1     COARSE ALTITUDE SYNCHRO (DEG)              CHGME     DEG     = (N/ 1000.0) -  100.0
21)   1     ALTIMETER SYNCHRO FINE ( DEG)              FHGME     DEG     = (N/ 1000.0) -  100.0
22)   1     HIGH RANGE R. ALTITUDE (APN-159) (M)       HGME       M      = (N/   10.0) -  500.0
23)   1     D-VALUE   (HGME-PALT) (M)                  DVALUE     M      = (N/   10.0) -10000.0
24)   1     GROUND SPEED (M/S)  (LR)            (M)     GSF1      M/S    = (N/ 1000.0) -    0.0
25)   1     RAW INS GROUND SPD EAST COMP(LR)  (M/S)    VEW1          M   = (N/ 1000.0) -  500.0
26)   1     RAW INS GROUND SPD NORTH COMP(LR) (M/S)    VNS1          M   = (N/ 1000.0) -  500.0
27)   1     DAMPED AIRCRAFT VERT VELOCITY(LR) (M/S)     WP3L      M/S    = (N/ 1000.0) -  100.0
28)   1     INS VERTICAL ACCELERATION(LR)    (M/S2)    ACZ1      M/S2    = (N/ 1000.0) -  100.0
29)   1     AIRCRAFT TRUE HEADING (YAW)(LR) (DEG)      THF1      DEG     = (N/ 1000.0) -  100.0
30)   1     AIRCRAFT ROLL ATTITUDE ANGLE(LR) (DEG)     ROLL1     DEG     = (N/ 1000.0) -  100.0
31)   1     AIRCRAFT PITCH ATTITUDE ANGLE(LR)(DEG)    PITCH1     DEG     = (N/ 1000.0) -  100.0
32)   1     AIRCRAFT TRUE AIRSPEED(BOOM)(LR)  (M/S)   TASB1       M/S    = (N/ 1000.0) -  100.0
33)   1     RAW IR SURF TEMP 9.5-11.5 MIC(PRT-5)(C)    PRT-5      C      = (N/ 1000.0) -  100.0
34)   1     RAW BOT. PYRANOM. OUTPUT(WG-7)(WATTS/M2)    BPYR1  WATTS/M2  = (N/  500.0) -  100.0
35)   1     RAW BOT. PYRANOM. OUTPUT(OG-1)(WATTS/M2)    BPYR2  WATTS/M2  = (N/  500.0) -  100.0
36)   1     RAW BOT. PYRANOM. OUTPUT(RG-8)(WATTS/M2)    BPYR3  WATTS/M2  = (N/  500.0) -  100.0
37)   1     RAW TOP PYRANOM. OUTPUT (WG-7)(WATTS/M2)    TPYR1  WATTS/M2  = (N/  500.0) -  100.0
38)   1     RAW TOP PYRANOM. OUTPUT (OG-1)(WATTS/M2)    TPYR2  WATTS/M2  = (N/  500.0) -  100.0
39)   1     RAW TOP PYRANOM. OUTPUT (RG-8)(WATTS/M2)    TPYR3  WATTS/M2  = (N/  500.0) -  100.0
40)   1     CORRECTED BOT. PYRGEOM. OUTPUT (WATTS/M2   BPYRGC   WATTS/M2 = (N/ 1000.0) -  100.0
41)   1     CORRECTED TOP PYRGEOM. OUTPUT (WATTS/M2)   TPYRGC   WATTS/M2 = (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     TOTAL TEMP.2 (BOOM ROSEM.ECTRON)(LR)(C)    TTB2L       C     = (N/ 1000.0) -  100.0
44)   1     TOTAL TEMP  (BOOM ROSEMOUNT)(LR)    (C)     TTB1       C     = (N/ 1000.0) -  100.0
45)   1     TOTAL TEMP. (DEICED ROSEMOUNT) (C)          TTFH       C     = (N/ 1000.0) -  100.0
46)   1     DEW/FROSTPOINT TEMP. TOP (EG&G) (C)        DPRT      C       = (N/ 1000.0) -  100.0
47)   1     DEW/FROSTPOINT TEMP BOT(EG&G)(C)           DPRB      C       = (N/ 1000.0) -  100.0
48)   1     RAW STATIC PRESSURE (WING)     (MB)        PSW1        MB    = (N/  500.0) -    0.0
49)   1     RAW DYNAMIC PRESSURE(WING)     (MB)        QCW1       MB     = (N/ 1000.0) -  100.0
50)   1     RAW STATIC PRESSURE (BOOM)     (MB)        PSB1        MB    = (N/  500.0) -    0.0
51)   1     RAW DYNAMIC PRESSURE (BOOM)(MB)(LR)        QCB1      MB      = (N/ 1000.0) -  100.0
52)   1     RAW INS LATITUDE (DEG)                    ALAT1    DEG       = (N/ 1000.0) -  200.0
53)   1     RAW INS LONGITUDE (DEG)                   ALONG1     DEG     = (N/ 1000.0) -  200.0
54)   1     INS WANDER ANGLE (DEG)                    ALPHA1     DEG     = (N/ 1000.0) -  100.0
55)   1     AIRCRAFT TRUE HEADING (LR)(ARINC)(DEG)     THI1      DEG     = (N/ 1000.0) -  100.0
56)   1     RAW BOTTOM PYRGEOMETER OUTPUT (WATTS/M2)    BPYRG  WATTS/M2  = (N/  100.0) - 1000.0
57)   1     RAW  TOP  PYRGEOMETER OUTPUT (WATTS/M2)     TPYRG  WATTS/M2  = (N/  100.0) - 1000.0
58)   1     BOTTOM PYRGEOMETER DOME TEMPERATURE (C)    BPGDT      C      = (N/ 1000.0) -  100.0
59)   1     BOTTOM PYRGEOMETER SINK TEMPERATURE (C)    BPGST      C      = (N/ 1000.0) -  100.0
60)   1     TOP PYRGEOMETER DOME TEMPERATURE (C)       TPGDT      C      = (N/ 1000.0) -  100.0
61)   1     TOP PYRGEOMETER SINK TEMPERATURE (C)       TPGST      C      = (N/ 1000.0) -  100.0
62)   1     RAW J-W LIQUID WATER CONTENT (G/M3)         LWC     G/M3     = (N/ 1000.0) -  100.0
63)  20     HORIZONTAL WIND DIRECTION         (DEG)  WDRCTN         DEG  = (N/ 1000.0) -    0.0
64)  20     HORIZONTAL WIND SPEED             (M/S)   WSPD          M/S  = (N/ 1000.0) -    0.0
65)  20     WIND VECTOR EAST GUST COMPONENT (M/S)        UI          M/S = (N/ 1000.0) -  200.0
66)  20     WIND VECTOR NORTH GUST COMPONENT (M/S)       VI          M/S = (N/ 1000.0) -  200.0
67)  20     WIND VECTOR VERTICAL GUST COMP.  (M/S)       WI          M/S = (N/ 1000.0) -  100.0
68)  20     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)   UX      M/S       = (N/ 1000.0) -  200.0
69)  20     WIND VECTOR LATERAL GUST COMPONENT (M/S)   VY      M/S       = (N/ 1000.0) -  200.0
70)  20      LYMAN-ALPHA FIXED PATH  (VDC)             VLA        VDC    = (N/ 1000.0) -  100.0
71)  20     TOTAL TEMP.2(BOOM ROSM.,ECTRON)(C)         TTB2      C       = (N/ 1000.0) -  100.0
72)  20     AMBIENT TEMP.2(BOOM ROSM. ECTRON)(C)      ATB2       C       = (N/ 1000.0) -  100.0
73)  20     RAW DYNAMIC PRESSURE (GUST PROBE) (MB)     QCG       MB      = (N/ 1000.0) -  100.0
74)  20     CORRECTED DYNAMIC PRESR (GUST PROBE)(MB)   QCGC      MB      = (N/ 1000.0) -  100.0
75)  20     AIRCRAFT TRUE AIRSPEED (GUST)(M/S)        TASG       M/S     = (N/ 1000.0) -  100.0
76)  20     ATTACK ANGLE (FIXED VANE LEFT SIDE)        AFIXL        DEG  = (N/ 1000.0) -  100.0
77)  20     ATTACK ANGLE (FIXED VANE RIGHT SIDE)       AFIXR        DEG  = (N/ 1000.0) -  100.0
78)  20     SIDE SLIP ANGLE (FIXED VANE TOP) (DEG)     BFIXT        DEG  = (N/ 1000.0) -  100.0
79)  20     SIDE SLIP ANGLE (FIXED VANE BOTTOM)        BFIXB        DEG  = (N/ 1000.0) -  100.0
80)  20     AIRCRAFT C.G.ACCELERATION(M/S2) (CH.18)    ACCG        M/S2  = (N/ 1000.0) -  100.0
81)  20     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/  100.0) - 5000.0
82)  20     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
83)  20     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
84)  20     AIRCRAFT TRUE HEADING    (DEG)             THF       DEG     = (N/ 1000.0) -  100.0
85)  20     RAW INS GROUND SPD X COMPONENT (M/S)        XVI       M/S    = (N/ 1000.0) -  500.0
86)  20     RAW INS GROUND SPD Y COMPONENT (M/S)        YVI       M/S    = (N/ 1000.0) -  500.0
87)  15     PMS PROBE 1 FSSP ( ACC.)                   PMSPB1    FSSP    = (N/ 1000.0) -  100.0
88)  15     PMS PROBE 2 200X ( ACC.)                   PMSPB2    200X    = (N/ 1000.0) -  100.0
89)  15     PMS PROBE 3 PMS3 ( ACC.)                   PMSPB3    PMS3    = (N/ 1000.0) -  100.0
90)   1     RELATIVE HUMIDITY  (PER CENT )             RHUM      PERCENT = (N/ 1000.0) -  100.0
91)   1     MIXING RATIO       (G/KG)                  RM        G/KG    = (N/ 1000.0) -  100.0
92)   1     EQUIVALENT POTENTIAL TEMP  (K)             ETHETA     K      = (N/ 1000.0) -  100.0
93)   1     POTENTIAL TEMPERATURE      (K)             THETA      K      = (N/ 1000.0) -  100.0
94)   1     OZONE DASIBI       (PPBV)                  DASIBI     PPBV   = (N/ 1000.0) -  100.0
95)   1     FHNO3                   (VDC)              FHNO3      VDC    = (N/ 1000.0) -  100.0
96)   1     RICE                    (VDC)              RICE       VDC    = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
805-03 ALPEX  HRT 06MAR1982
THIS FILE IS ALL OR PART OF THE TIME PERIOD  9        49        45         TO   17         4         0
DESCRIPTION OF TAPE:
HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
605 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
503360 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 11880 BITS PER LOGICAL DATA RECORD
2 LOGICAL DATA RECORDS PER PHYSICAL RECORD
23760 BITS PER PHYSICAL DATA RECORD
PROJECT FLIGHT DATE HRT 0AR
PROJECT FLIGHT TIME  9  49  54
MACHINE = 7600
96 PARAMETERS WERE SAVED AT THEIR RESPECTIVE RATES
594 SAMPLES WERE SCALED INTO 20 BIT INTEGER WORDS.```