Sample HRT GENPRO-I header

  NCAR ELECTRA - OAFSS - 7 MARCH 1975               FIRST TIME ON THIS FILE 20 17 12       THIS FILE I
  S ALL OR PART OF TIME PERIOD 20 17 12 TO 25 11 33  DESCRIPTION OF RECORD -- 115 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  786 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  2 CYCLES OF 786 SAMP/CYC = 1572 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 524 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     TIME                                        TIME     SECONDS = (N/      1) -    0.0
    2)   1     UNALTERED TAPE TIME (SECONDS)               TPTIME SECONDS   = (N/      1) -    0.0
    3)   1     CORRECTED STATIC PRESSURE (MB)               PSWC    (MB)    = (N/    500) -    0.0
    4)   1     AMBIENT TEMPERATURE (ROSEMOUNT) (C)          ATF     (C)     = (N/   1000) -  100.0
    5)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
    6)   1     DEWPOINT TEMPERATURE (THERMOELEC) (C)      DPRHC     (C)     = (N/   1000) -  100.0
    7)   1     DEWPOINT TEMPERATURE (LYMN-ALPHA) (C)     DPLAC      (C)     = (N/   1000) -  100.0
    8)   1     ABSOLUTE HUMIDITY (THERMOELEC) (GM/M3)      RHOTD    (GM/M3) = (N/   1000) -  100.0
    9)   1     ABSOLUTE HUMIDITY (LYMN-ALPHA) (GM/M3)      RHOLY    (GM/M3) = (N/   1000) -  100.0
   10)   1     HORIZONTAL WIND DIRECTION (DEG)             WDRCTN   (DEG)   = (N/   1000) -    0.0
   11)   1     HORIZONTAL WIND SPEED (M/S)                  WSPD    (M/S)   = (N/   1000) -    0.0
   12)   1     WIND VECTOR EAST COMPONENT (M/S)               UI1   (M/S)   = (N/   1000) -  200.0
   13)   1     WIND VECTOR NORTH COMPONENT (M/S)              VI1   (M/S)   = (N/   1000) -  200.0
   14)   1     WIND VECTOR VERT GUST COMPONENT (M/S)          WI1   (M/S)   = (N/   1000) -  100.0
   15)   1     WIND VECTOR LNGTDNL COMPONENT (M/S)            UX1   (M/S)   = (N/   1000) -  200.0
   16)   1     WIND VECTOR LATERAL COMPONENT (M/S)            VY1   (M/S)   = (N/   1000) -  200.0
   17)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   18)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   19)   1     NACA PRESSURE ALTITUDE (M)                   HP      (M)     = (N/    100) -  100.0
   20)   1     PRESSURE DAMPED INERTIAL ALTITUDE (M)          HI31  (M)     = (N/    100) -  100.0
   21)   1     GEOMETRIC (RADIO) ALTITUDE (M)               HGM     (M)     = (N/   1000) -  100.0
   22)   1     AIRCRAFT GROUND SPEED (M/S)                 GS       (M/S)   = (N/   1000) -    0.0
   23)   1     AIRCRAFT GROUND SPD EAST COMP (M/S)            VEW   (M/S)   = (N/   1000) -  500.0
   24)   1     AIRCRAFT GROUND SPD NORTH COMP (M/S)           VNS   (M/S)   = (N/   1000) -  500.0
   25)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)          WP31    (M/S)   = (N/   1000) -  100.0
   26)   1     AIRCRAFT C.G. VERT ACCELERATION (M/S2)      CGAC1    (M/S2)  = (N/   1000) -  100.0
   27)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)            THF1    (DEG)   = (N/   1000) -    0.0
   28)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)          ROLL1    (DEG)   = (N/   1000) -  100.0
   29)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)         PITCH1   (DEG)   = (N/   1000) -  100.0
   30)   1     AIRCRAFT TRUE AIRSPEED (M/S)                 TASW    (M/S)   = (N/   1000) -  100.0
   31)   1     CORCTD IR SURFACE TEMP (PRT-5) (C)          PRT5C    (C)     = (N/   1000) -  100.0
   32)   1     DOWNWARD SW/WG-7 IRRADIANCE (WATTS/M2)      UPYR1  WATTS/M2  = (N/    500) -  100.0
   33)   1     DOWNWARD SW/OG-1 IRRADIANCE (WATTS/M2)      UPYR2  WATTS/M2  = (N/    500) -  100.0
   34)   1     DOWNWARD SW/RG-8 IRRADIANCE (WATTS/M2)      UPYR3  WATTS/M2  = (N/    500) -  100.0
   35)   1     UPWARD SW/WG-7 IRRADIANCE (WATTS/M2)        LPYR1  WATTS/M2  = (N/    500) -  100.0
   36)   1     UPWARD SW/OG-1 IRRADIANCE (WATTS/M2)        LPYR2  WATTS/M2  = (N/    500) -  100.0
   37)   1     UPWARD SW/RG-8 IRRADIANCE (WATTS/M2)        LPYR3  WATTS/M2  = (N/    500) -  100.0
   38)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   39)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   40)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   41)   1     PRT-6 FILTER POSITION                       P6FP             = (N/      1) -    0.0
   42)   1     PRT-6 MIRROR POSITION (DEG)                 P6MP      (DEG)  = (N/   1000) -  100.0
   43)   1     CORCTD J-W LIQUID WATER CONTENT (GM/M3)      LWCC   (GM/M3)  = (N/   1000) -  100.0
   44)   1     NOSEBOOM TOTAL TEMP (ROSEMOUNT) (C)           TTB5     DEG C = (N/   1000) -  100.0
   45)   1     FUSELAGE TOTAL TEMP (ROSEMOUNT) (C)           TTF    (C)     = (N/   1000) -  100.0
   46)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   47)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   48)   1     RHS DEW/FROSTPOINT TEMP (C)                   DPRH   (C)     = (N/   1000) -  100.0
   49)   1     LYMAN-ALPHA GAIN INDICATOR (VDC)           LAGAIN    (VDC)   = (N/   1000) -  100.0
   50)   1     RAW WINGTIP STATIC PRESSURE (MB)              PSW    (MB)    = (N/    500) -    0.0
   51)   1     RAW WINGTIP DYNAMIC PRESSURE (MB)             QCW    (MB)    = (N/   1000) -  100.0
   52)   1     RAW NOSEBOOM STATIC PRESSURE (MB)             PSB    (MB)    = (N/    500) -    0.0
   53)   1     RAW NOSEBOOM DYNAMIC PRESSURE (MB)            QCB    (MB)    = (N/   1000) -  100.0
   54)   1     RAW INS LATITUDE (DEG)                        ALAT   (DEG)   = (N/   1000) -  200.0
   55)   1     RAW INS LONGITUDE (DEG)                      ALONG   (DEG)   = (N/   1000) -  200.0
   56)   1     RAW VLF LATITUDE (DEG)                        VLAT    (DEG)  = (N/   1000) -  200.0
   57)   1     RAW VLF LONGITUDE (DEG)                      VLONG   (DEG)   = (N/   1000) -  200.0
   58)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   59)   1     INS WANDER ANGLE (DEG)                       ALPHA   (DEG)   = (N/   1000) -  100.0
   60)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)           THI    (DEG)   = (N/   1000) -  100.0
   61)   1     RAW DWNWARD IR IRRADIANCE (WATTS/M2)       UPYRG   WATTS/M2  = (N/    100) - 1000.0
   62)   1     RAW UPWARD IR IRRADIANCE (WATTS/M2)        LPYRG   WATTS/M2  = (N/    100) - 1000.0
   63)   1     UPPER PYRGEOMETER DOME TEMP (C)             UPYRWT   (C)     = (N/   1000) -  100.0
   64)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   65)   1     LOWER PYRGEOMETER DOME TEMP (C)             LPYRWT   (C)     = (N/   1000) -  100.0
   66)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   67)   1     PRT-5 IRTRAN WINDOW TEMP (C)               PRT5WT    (C)     = (N/   1000) -  100.0
   68)   1     RAW IR SURFACE TEMP(PRT-5) (C)                PRT5   (C)     = (N/   1000) -  100.0
   69)   1     PRT-6 RADIOMETER OUTPUT VOLTAGE (VDC)       P6RADV    (C)    = (N/   1000) -  100.0
   70)   1     PRT-6 OVEN DEVIATION TEMP (C)               P6OVNT  (C)      = (N/   1000) -  100.0
   71)   1     PRT-6 ROTATING MIRROR TEMP (DEG)            P6RMT     (C)    = (N/   1000) -  100.0
   72)   1     PRT-6 FIXED MIRROR TEMP (C)                 P6FMT     (C)    = (N/   1000) -  100.0
   73)   1     PRT-6 CALIBRATION PLATE TEMP (C)            P6CPT     (C)    = (N/   1000) -  100.0
   74)   1     PRT-6 MODE VOLTAGE (VDC)                    P6MV     (VDC)   = (N/      1) -    0.0
   75)   1     RAW J-W LIQUID WATER CONTENT (GM/M3)         LWC     (GM/M3) = (N/   1000) -  100.0
   76)   1     16MM CAMERA FRAME COUNT                    CAMFC             = (N/      1) -    0.0
   77)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   78)   1     INS/KNLBRG UPDATE FLAGS                     UPDATE           = (N/      1) -    0.0
   79)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   80)  20     AMBIENT TEMPERATURE (FAST RESPONSE) (C)     ATKPA    (C)     = (N/   1000) -  100.0
   81)  20               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   82)  20               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   83)  20     WIND VECTOR EAST GUST COMPONENT (M/S)           UI   (M/S)   = (N/   1000) -  200.0
   84)  20     WIND VECTOR NORTH GUST COMPONENT (M/S)          VI   (M/S)   = (N/   1000) -  200.0
   85)  20     WIND VECTOR VERT GUST COMPONENT (M/S)           WI   (M/S)   = (N/   1000) -  100.0
   86)  20     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)        UX   (M/S)   = (N/   1000) -  200.0
   87)  20     WIND VECTOR LATERAL GUST COMPONENT (M/S)        VY   (M/S)   = (N/   1000) -  200.0
   88)  20     ABSOLUTE HUMIDITY (REFRACT) (GM/M3)          RHORF   (GM/M3) = (N/   1000) -  100.0
   89)  20     ABSOLUTE HUMIDITY (LYMN-ALPHA) (GM/M3)       RHOLA   (GM/M3) = (N/   1000) -  100.0
   90)  20     REFRACTIVE INDEX (N UNITS)                    RFI (N UNITS)  = (N/   1000) -    0.0
   91)  20     LYMAN-ALPHA HYGROMETER OUTPUT (VDC)          LAV     (VDC)   = (N/   1000) -  100.0
   92)  20     FAST RESPONSE TOTAL TEMP (C)                 TTKP    (C)     = (N/   1000) -  100.0
   93)  20     NOSE ROSEMOUNT TOTAL TEMP (C)                 TTB    (C)     = (N/   1000) -  100.0
   94)  20     RAW GUST PROBE DYNAMIC PRESSURE (MB)          QCG    (MB)    = (N/   1000) -  100.0
   95)  20     ATTACK ANGLE - ROTATING VANE (DEG)         ATKR      (DEG)   = (N/   1000) -  100.0
   96)  20     ATTACK ANGLE - FIXED VANE (DEG)               AFIX   (DEG)   = (N/   1000) -  100.0
   97)  20     SIDESLIP ANGLE - ROTATING VANE (DEG)       BTAR      (DEG)   = (N/   1000) -  100.0
   98)  20     SIDESLIP ANGLE - FIXED VANE (DEG)             BFIX   (DEG)   = (N/   1000) -  100.0
   99)  20     GUST PROBE TIP VERT ACCEL (M/S2)               VAC   (M/S2)  = (N/   1000) -  100.0
  100)  20     GUST PROBE TIP LATERAL ACCEL (M/S2)            LAC   (M/S2)  = (N/   1000) -  100.0
  101)  20     AIRCRAFT C.G. VERT ACCELERATION (M/S2)       CGAC    (M/S2)  = (N/   1000) -  100.0
  102)  20     RAW INS VERTICAL VELOCITY (M/S)              VZI     (M/S)   = (N/    100) - 5000.0
  103)  20     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)            ROLL   (DEG)   = (N/   1000) -  100.0
  104)  20     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)          PITCH   (DEG)   = (N/   1000) -  100.0
  105)  20     AIRCRAFT TRUE HEADING (YAW) (DEG)             THF    (DEG)   = (N/   1000) -  100.0
  106)  20     RAW INS GROUND SPD X COMPONENT (M/S)         XVI     (M/S)   = (N/   1000) -  500.0
  107)  20     RAW INS GROUND SPD Y COMPONENT (M/S)         YVI     (M/S)   = (N/   1000) -  500.0
  108)  20            LEFT WING STRAIN (MICRO-IN/IN)        STRLW (UIN/IN)  = (N/    500) - 1000.0
  109)  20            RIGHT WING STRAIN (MICRO-IN/IN)       STRRW (UIN/IN)  = (N/    500) - 1000.0
  110)  64     KNOLLENBERG 64 WORDS                      KNLBG       COUNTS = (N/      1) -    0.0
  111)   1     SPACE CHARGE AIRFLOW (LATHAM) (VDC)       SCAF       (VDC)   = (N/   1000) -  100.0
  112)   1     FLUSH MILL - SUM (LATHAM) (VDC)              FMS     (VDC)   = (N/   1000) -  100.0
  113)   1     FLUSH MILL - DIFF (LATHAM) (VDC)             FMD1    (VDC)   = (N/   1000) -  100.0
  114)  20     FLUSH MILL - DIFF (LATHAM) (VDC)             FMD     (VDC)   = (N/   1000) -  100.0
  115)  20     SPACE CHARGE (LATHAM) (VDC)                  SC      (VDC)   = (N/   1000) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  NCAR ELECTRA - OAFSS - 7 MARCH 1975
 THIS FILE IS ALL OR PART OF THE TIME PERIOD 20        17        12         TO   25        11        33
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                          797 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                       663104 BITS PER PHYSICAL HEADER RECORD
           DATA FILE -- 15720 BITS PER LOGICAL DATA RECORD
                            2 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        31440 BITS PER PHYSICAL DATA RECORD