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.