Sample HRT GENPRO-I header

   886-01 ARCTIC STRATUS 13JUN80 18 19 20           FIRST TIME ON THIS FILE 18 19 25       THIS FILE I
  S ALL OR PART OF TIME PERIOD 18 19 20 TO 24 25 30  DESCRIPTION OF RECORD -- 113 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  615 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  2 CYCLES OF 615 SAMP/CYC = 1230 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 410 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     DEWPOINT TEMPERATURE (THERM.)(TOP) (C)     DPRTC     C       = (N/ 1000.0) -  100.0
    6)   1     DEWPOINT TEMPERATURE (THERM.)(BOT.)(C)     DPRBC     C       = (N/ 1000.0) -  100.0
    7)   1     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)      RHOTD     G/M3    = (N/ 1000.0) -  100.0
    8)   1     HORIZONTAL WIND DIRECTION (LR)(DEG)        WDRCTN1       DEG = (N/ 1000.0) -    0.0
    9)   1     HORIZONTAL WIND SPEED (LR)(M/S)           WSPD1          M/S = (N/ 1000.0) -    0.0
   10)   1     WIND VECTOR EAST COMPONENT (LR)(M/S)         UI1        M/S  = (N/ 1000.0) -  200.0
   11)   1     WIND VECTOR NORTH COMPONENT(LR) (M/S)        VI1        M/S  = (N/ 1000.0) -  200.0
   12)   1     WIND VECTOR VERTICAL GUST COMP(LR)(M/S)      WI1        M/S  = (N/ 1000.0) -  100.0
   13)   1     WIND VECTOR LNGTDNL  COMP.(LR)(M/S)        UX1     M/S       = (N/ 1000.0) -  200.0
   14)   1     WIND VECTOR LATERAL  COMP.(LR)1(M/S)       VY1     M/S       = (N/ 1000.0) -  200.0
   15)   1     NACA PRESSURE ALTITUDE (LR) (M)             HP1       M      = (N/   10.0) -  500.0
   16)   1     PRESSURE-DAMPED INERTIAL ALTITUDE(LR)(M)    HI31       M     = (N/   10.0) -  500.0
   17)   1     COARSE ALTITUDE SYNCHRO (DEG)              CHGME     DEG     = (N/ 1000.0) -  100.0
   18)   1     FINE ALTITUDE SYNCHRO (DEG)                HGME      DEG     = (N/ 1000.0) -  100.0
   19)   1     ALTITUDE (M) (APN-159)                     ALT        M      = (N/   10.0) -  500.0
   20)   1     RAW INS GROUND SPD EAST COMP.(LR)(M/S)         VEW1      M   = (N/ 1000.0) -  500.0
   21)   1     RAW INS GROUND SPD NORTH COMP.(LR)(M/S)        VNS1      M   = (N/ 1000.0) -  500.0
   22)   1     DAMPED AIRCRAFT VERT VELOCITY(LR)(M/S)      WP31      M/S    = (N/ 1000.0) -  100.0
   23)   1     AIRCRAFT C.G. ACCELERATION (LR)(M/S2)      CGAC1     M/S2    = (N/ 1000.0) -  100.0
   24)   1     AIRCRAFT TRUE HEADING (YAW)(LR) (DEG)      THF1      DEG     = (N/ 1000.0) -    0.0
   25)   1     AIRCRAFT ROLL ATTITUDE ANGLE(LR) (DEG)     ROLL1     DEG     = (N/ 1000.0) -  100.0
   26)   1     AIRCRAFT PITCH ATTITUDE ANGLE(LR)(DEG)     PITCH1    DEG     = (N/ 1000.0) -  100.0
   27)   1     AIRCRAFT TRUE AIRSPEED (WING) (M/S)           TASW1    M/S   = (N/ 1000.0) -  100.0
   28)   1     RAW RADIOMETRIC SURFACE TEMP (PRT-5) (C)   PRT-5      C      = (N/ 1000.0) -  100.0
   29)   1     RAW BOTTOM PYRANOMETER OUTPUT (WG-7) (WA    BPYR1  WATTS/M2  = (N/  500.0) -  100.0
   30)   1     RAW BOTTOM PYRANOMETER OUTPUT (OG-1) (WA    BPYR2  WATTS/M2  = (N/  500.0) -  100.0
   31)   1     RAW BOTTOM PYRANOMETER OUTPUT (RG-8) (WA    BPYR3  WATTS/M2  = (N/  500.0) -  100.0
   32)   1     RAW  TOP  PYRANOMETER OUTPUT (WG-7) (WAT    TPYR1  WATTS/M2  = (N/  500.0) -  100.0
   33)   1     RAW  TOP  PYRANOMETER OUTPUT (RG-8) (WAT    TPYR2  WATTS/M2  = (N/  500.0) -  100.0
   34)   1     RAW  TOP  PYRANOMETER OUTPUT (RG-8) (WAT    TPYR3  WATTS/M2  = (N/  500.0) -  100.0
   35)   1     CORRECTED BOTTOM PYRGEOMETER OUTPUT (WAT   BPYRGC   WATTS/M2 = (N/ 1000.0) -  100.0
   36)   1     CORRECTED  TOP  PYRGEOMETER OUTPUT (WATT   TPYRGC   WATTS/M2 = (N/ 1000.0) -  100.0
   37)   1     CORRCTD J-W LIQUID WATER CONTENT (G/M3)    LWCC      G/M3    = (N/ 1000.0) -  100.0
   38)   1     TOTAL TEMPERATURE(BOOM ROSMT)(LR)(C)        TTB1       C     = (N/ 1000.0) -  100.0
   39)   1     DEW/FROSTPOINT TEMP (TOP) (C)              DPRT      C       = (N/ 1000.0) -  100.0
   40)   1     DEW/FROSTPOINT TEMP (BOT.) (C)             DPRB      C       = (N/ 1000.0) -  100.0
   41)   1     RAW DYNAMIC PRESSURE (WING)(LR)(MB)           PSW1     MB    = (N/  500.0) -    0.0
   42)   1     RAW DYNAMIC PRESSURE(WING)(LR)(MB)            QCW1    MB     = (N/ 1000.0) -  100.0
   43)   1     RAW STATIC PRESSURE (BOOM)(LR) (MB)           PSB1     MB    = (N/  500.0) -    0.0
   44)   1     RAW DYNAMIC PRESSURE (LR) (BOOM) (MB)         QCB1    MB     = (N/ 1000.0) -  100.0
   45)   1     RAW INS LATITUDE (DEG)                        ALAT     DEG   = (N/ 1000.0) -  200.0
   46)   1     RAW INS LONGITUDE (DEG)                      ALONG     DEG   = (N/ 1000.0) -  200.0
   47)   1     INS WANDER ANGLE (DEG) (LR)                  ALPHA1     DEG  = (N/ 1000.0) -  100.0
   48)   1     AIRCRAFT TRUE HEADING (LR)(ARINC)(DEG)       THI1       DEG  = (N/ 1000.0) -  100.0
   49)   1     RAW BOTTOM PYRGEOMETER OUTPUT (WATTS/M2)    BPYRG  WATTS/M2  = (N/  100.0) - 1000.0
   50)   1     RAW  TOP  PYRGEOMETER OUTPUT (WATTS/M2)     TPYRG  WATTS/M2  = (N/  100.0) - 1000.0
   51)   1     BOTTOM PYRGEOMETER DOME TEMPERATURE (C)    BPGDT      C      = (N/ 1000.0) -  100.0
   52)   1     BOTTOM PYRGEOMETER SINK TEMPERATURE (C)    BPGST      C      = (N/ 1000.0) -  100.0
   53)   1     TOP PYRGEOMETER DOME TEMPERATURE (C)       TPGDT      C      = (N/ 1000.0) -  100.0
   54)   1     TOP PYRGEOMETER SINK TEMPERATURE (C)       TPGST      C      = (N/ 1000.0) -  100.0
   55)   1     PRT-6 OVEN TEMP DEVIATION (VDC)            P6OVNT    VDC     = (N/ 1000.0) -  100.0
   56)   1     FMP MARK 1 VOLTAGE (VDC)                   MK1T      VDC     = (N/ 1000.0) -  100.0
   57)   1     PRT-6 ROTATING MIRROR TEMP (VDC)           P6RMT     VDC     = (N/ 1000.0) -  100.0
   58)   1     PRT-6 FIXED MIRROR TEMP (VDC)              P6FMT     VDC     = (N/ 1000.0) -  100.0
   59)   1     PRT-6 CALIBRATION PLATE TEMP(VDC)          P6CPT     VDC     = (N/ 1000.0) -  100.0
   60)   1       FMP MARK 2 VOLTAGE                       MK2T      VDC     = (N/ 1000.0) -  100.0
   61)   1     FMT MARK 1 VOLTAGE (VDC)                   MK1       VDC     = (N/ 1000.0) -  100.0
   62)   1     PRT-6 FILTER POSITION                      P6FP      VDC     = (N/ 1000.0) -  100.0
   63)   1     PRT-6 MIRROR POSITION (VDC)                P6MP      VDC     = (N/ 1000.0) -  100.0
   64)   1     PRT-6 MODE INDICATOR                       P6MV      VDC     = (N/ 1000.0) -  100.0
   65)   1       FMT MARK 2 VOLTAGE                       MK2       VDC     = (N/ 1000.0) -  100.0
   66)   1     PRT-6 RADIOMETER OUTPUT VOLTAGE (VDC)      P6RADV    VDC     = (N/ 1000.0) -  100.0
   67)   1     RAW J-W LIQUID WATER CONTENT (G/M3)         LWC     G/M3     = (N/ 1000.0) -  100.0
   68)   5     PRT-6 OVEN TEMP DEVIATION (VDC)            P6OVNT    VDC     = (N/ 1000.0) -  100.0
   69)   5     PRT-6 ALL MUX. TEMPERATURE (VDC)           MUXTEMP   VDC     = (N/ 1000.0) -  100.0
   70)   5     PRT-6 ALL MUX. POSITION (VDC)              MUXPOS    VDC     = (N/ 1000.0) -  100.0
   71)   5     PRT-6 RADIOMETER OUTPUT VOLTAGE (VDC)      P6RADV    VDC     = (N/ 1000.0) -  100.0
   72)  20     AMBIENT TEMP. (COMP. BOOM) (C)               ATBC      C     = (N/ 1000.0) -  100.0
   73)  20     AMBIENT TEMPERATURE(FAST RESPONSE) (C)       ATKP      C     = (N/ 1000.0) -  100.0
   74)  20     WIND VECTOR EAST GUST COMPONENT (M/S)        UI          M/S = (N/ 1000.0) -  200.0
   75)  20     WIND VECTOR NORTH GUST COMPONENT (M/S)       VI          M/S = (N/ 1000.0) -  200.0
   76)  20     WIND VECTOR VERTICAL GUST COMP.  (M/S)       WI          M/S = (N/ 1000.0) -  100.0
   77)  20     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)   UX      M/S       = (N/ 1000.0) -  200.0
   78)  20     WIND VECTOR LATERAL GUST COMPONENT (M/S)   VY      M/S       = (N/ 1000.0) -  200.0
   79)  20     DAMPED AIRCRAFT VERT VELOCITY (M/S)         WP3       M/S    = (N/ 1000.0) -  100.0
   80)  20     FIXED PATH LYMAN-ALPHA (VDC)               VLAFP      VDC    = (N/ 1000.0) -  100.0
   81)  20     TOTAL TEMPERATURE (FAST RESPONSE) (C)      TTKP      C       = (N/ 1000.0) -  100.0
   82)  20     TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C)      TTB        C     = (N/ 1000.0) -  100.0
   83)  20     TOTAL TEMP. (COMP. BOOM ROSEMOUNT) (C)      TTBC       C     = (N/ 1000.0) -  100.0
   84)  20     RAW DYNAMIC PRESSURE (GUST PROBE) (MB)     QCG       MB      = (N/ 1000.0) -  100.0
   85)  20     ATTACK ANGLE (FIXED VANE 1) (DEG)          AFIX         DEG  = (N/ 1000.0) -  100.0
   86)  20     SIDE SLIP ANGLE (FIXED VANE 1) (DEG)       BFIX         DEG  = (N/ 1000.0) -  100.0
   87)  20     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   88)  20     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/  100.0) - 5000.0
   89)  20     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
   90)  20     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
   91)  20     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
   92)  20     RAW INS GROUND SPD X COMPONENT (M/S)        XVI       M/S    = (N/ 1000.0) -  500.0
   93)  20     RAW INS GROUND SPD Y COMPONENT (M/S)        YVI       M/S    = (N/ 1000.0) -  500.0
   94)  20     AIRCRAFT GROUND SPEED   (M/S)               GSF       M/S    = (N/ 1000.0) -  100.0
   95)  20     AIRCRAFT TRUE AIRSPEED (GUST PROBE)(M/S)    TASGB      M/S   = (N/ 1000.0) -  100.0
   96)  16     PMS PROBE 1 FSSP (ID AND ACC.)             PMSPB1    FSSP    = (N/    1.0) -    0.0
   97)  16     PMS PROBE 2 200X (ID AND ACC.)             PMSPB2    200X    = (N/    1.0) -    0.0
   98)   1     EVENT MARKER WORD                          EVMRKS            = (N/ 1000.0) -  100.0
   99)   1      HRMN 01 (VDC)                            HRMN1       VDC    = (N/ 1000.0) -  100.0
  100)   1      HRMN 02 (VDC)                            HRMN2       VDC    = (N/ 1000.0) -  100.0
  101)   1      HRMN 03 (VDC)                            HRMN3       VDC    = (N/ 1000.0) -  100.0
  102)   1      HRMN 04 (VDC)                            HRMN4       VDC    = (N/ 1000.0) -  100.0
  103)   1      HRMN 05 (VDC)                            HRMN5       VDC    = (N/ 1000.0) -  100.0
  104)   1      HRMN 06 (VDC)                            HRMN6       VDC    = (N/ 1000.0) -  100.0
  105)   1      HRMN 07 (VDC)                            HRMN7       VDC    = (N/ 1000.0) -  100.0
  106)   1      HRMN 08 (VDC)                            HRMN8       VDC    = (N/ 1000.0) -  100.0
  107)   1      HRMN 09 (VDC)                            HRMN9       VDC    = (N/ 1000.0) -  100.0
  108)   1      HRMN 10 (VDC)                            HRMN10      VDC    = (N/ 1000.0) -  100.0
  109)   1      HRMN 11 (VDC)                            HRMN11      VDC    = (N/ 1000.0) -  100.0
  110)   1      HRMN 12 (VDC)                            HRMN12      VDC    = (N/ 1000.0) -  100.0
  111)   1      HRMN 13 (VDC)                            HRMN13      VDC    = (N/ 1000.0) -  100.0
  112)   1      HRMN 14 (VDC)                            HRMN14      VDC    = (N/ 1000.0) -  100.0
  113)   1      HRMN 15 (VDC)                            HRMN15      VDC    = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
   886-01 ARCTIC STRATUS 13JUN80 18 19 20
 THIS FILE IS ALL OR PART OF THE TIME PERIOD 18        19        20         TO   24        25        30
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                          626 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                       520832 BITS PER PHYSICAL HEADER RECORD
           DATA FILE -- 12300 BITS PER LOGICAL DATA RECORD
                            2 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        24600 BITS PER PHYSICAL DATA RECORD