sample GENPRO-I header
  691A-1  ZOLLER - POWER PLANT PLUMES 2  15AUG76    FIRST TIME ON THIS FILE 08 42 10       THIS FILE I
  S ALL OR PART OF TIME PERIOD 08 42 10 TO 10 53 23  DESCRIPTION OF RECORD --  55 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS   55 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE 27 CYCLES OF  55 SAMP/CYC = 1485 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 495 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 (MB)             PSFC      MB      = (N/ 1000.0) -    0.0
    4)   1     AMBIENT TEMPERATURE (ROSEMOUNT) (C)        ATW       C       = (N/ 1000.0) -  100.0
    5)   1     AMBIENT TEMPERATURE (REVERSE-FLOW) (C)     ATRF      C       = (N/ 1000.0) -  100.0
    6)   1     DEWPOINT TEMPERATURE (THERMOELEC) (C)      DPC       C       = (N/ 1000.0) -  100.0
    7)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
    8)   1     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)      RHOTD     G/M3    = (N/ 1000.0) -  100.0
    9)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   10)   1     HORIZONTAL WIND DIRECTION (DEG)            WDRCTN    DEG     = (N/ 1000.0) -  100.0
   11)   1     HORIZONTAL WIND SPEED (M/S)                WSPD      M/S     = (N/ 1000.0) -  100.0
   12)   1     WIND VECTOR EAST COMPONENT (M/S)           UI1       M/S     = (N/ 1000.0) -  200.0
   13)   1     WIND VECTOR NORTH COMPONENT (M/S)          VI1       M/S     = (N/ 1000.0) -  200.0
   14)   1     WIND VECTOR LNGTDNL COMPONENT (M/S)        UX1       M/S     = (N/ 1000.0) -  200.0
   15)   1     WIND VECTOR LATERAL COMPONENT (M/S)        VY1       M/S     = (N/ 1000.0) -  200.0
   16)   1     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
   17)   1     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
   18)   1     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
   19)   1     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
   20)   1     GEOMETRIC (RADIO) ALTITUDE (M)             HGM       M       = (N/ 1000.0) -  100.0
   21)   1     RAW INS GROUND SPEED (M/S)                 GSF       M/S     = (N/ 1000.0) -  100.0
   22)   1     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
   23)   1     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
   24)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
   25)   1     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   26)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
   27)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
   28)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
   29)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   30)   1     AIRCRAFT TRUE AIRSPEED (WING) (M/S)        TASW      M/S     = (N/ 1000.0) -  100.0
   31)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   32)   1     DISTANCE EAST OF START (KM)                DEI       KM      = (N/  100.0) - 1000.0
   33)   1     DISTANCE NORTH OF START (KM)               DNI       KM      = (N/  100.0) - 1000.0
   34)   1     TOTAL TEMPERATURE (WING ROSEMOUNT) (C)     TTW       C       = (N/ 1000.0) -  100.0
   35)   1     TOTAL TEMPERATURE (REVERSE FLOW) (C)       TTRF      C       = (N/ 1000.0) -  100.0
   36)   1     DEW/FROSTPOINT TEMP (THERMOELEC) (C)       DP        C       = (N/ 1000.0) -  100.0
   37)   1     RAW FUSELAGE STATIC PRESSURE (MB)          PSF       MB      = (N/ 1000.0) -    0.0
   38)   1     RAW WING DYNAMIC PRESSURE (MB)             QCW       MB      = (N/ 1000.0) -  100.0
   39)   1     ?                                          ?         ?       = ?
   40)   1     ?                                          ?         ?       = ?
   41)   1     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
   42)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
   43)   1     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
   44)   1     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
   45)   1     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
   46)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   47)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   48)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   49)   1     EVENT MARKER WORD                          EVMRKS            = (N/    1.0) -    0.0
   50)   1     FIXED ZERO VOLTAGE (VDC)                   FZV       VDC     = (N/ 1000.0) -  100.0
   51)   1               *** UNUSED ***                   UNUSED            = (N/      1) -    0.0
   52)   1     CONDENSATION NUCLEI (VOLTS)                CN        VDC     = (N/ 1000.0) -  100.0
   53)   1     SULFUR GAS (VOLTS)                         SO2       VDC     = (N/ 1000.0) -  100.0
   54)   1     OZONE (VOLTS)                              O3        VDC     = (N/ 1000.0) -  100.0
   55)   1     RELATIVE HUMIDITY (PER CENT)               RHUM      PER CENT= (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  697A-1  ZOLLER - POWER PLANT PLUME 2 15AUG76
 THIS FILE IS ALL OR PART OF THE TIME PERIOD  8        42        10         TO   10        53        23
 DESCRIPTION OF TAPE:
         HEADER FILE --     ? BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                            ? LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                            ? BITS PER PHYSICAL HEADER RECORD
           DATA FILE --  1100 BITS PER LOGICAL DATA RECORD
                           27 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        29700 BITS PER PHYSICAL DATA RECORD