Sample LRT GENPRO-I header

  646-01  SEA SALT NUCLEI 12JAN79 14/31/30          FIRST TIME ON THIS FILE 14 31 30       THIS FILE I
  S ALL OR PART OF TIME PERIOD 14 31 30 TO 17 13  0  DESCRIPTION OF RECORD --  66 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS   66 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE 22 CYCLES OF  66 SAMP/CYC = 1452 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 484 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     LTN-51 ARINC TIME LAG (SEC)                TMLAG     SEC     = (N/ 1000.0) -  100.0
    4)   1     EVENT MARKER WORD                          EVMRKS            = (N/    1.0) -    0.0
    5)   1     FIXED ZERO VOLTAGE (VDC)                   FZV       VDC     = (N/ 1000.0) -  100.0
    6)   1     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
    7)   1     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
    8)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
    9)   1     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
   10)   1     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
   11)   1     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
   12)   1     RAW INS GROUND SPEED (M/S)                 GSF       M/S     = (N/ 1000.0) -  100.0
   13)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
   14)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
   15)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
   16)   1     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
   17)   1     RAW DYNAMIC PRESSURE (WING) (MB)           QCW       MB      = (N/ 1000.0) -  100.0
   18)   1     RAW DYNAMIC PRESSURE (GUST PROBE) (MB)     QCG       MB      = (N/ 1000.0) -  100.0
   19)   1     CORRECTED DYNAMIC PRESR (WING)  (MB)       QCWC      MB      = (N/ 1000.0) -  100.0
   20)   1     CORRECTED DYNAMIC PRESR (GUST PROBE)(MB)   QCGC      MB      = (N/ 1000.0) -  100.0
   21)   1     RAW STATIC PRESSURE (FUSELAGE) (MB)        PSF       MB      = (N/ 1000.0) -    0.0
   22)   1     RAW STATIC PRESSURE (BOOM) (MB)            PSB       MB      = (N/ 1000.0) -    0.0
   23)   1     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
   24)   1     CORRECTED STATIC PRESSURE (BOOM) (MB)      PSBC      MB      = (N/ 1000.0) -    0.0
   25)   1     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
   26)   1     GEOMETRIC (RADIO) ALTITUDE (M)             HGM       M       = (N/ 1000.0) -  100.0
   27)   1     TOTAL TEMPERATURE (WING ROSEMOUNT) (C)     TTW       C       = (N/ 1000.0) -  100.0
   28)   1     TOTAL TEMPERATURE (REVERSE FLOW) (C)       TTRF      C       = (N/ 1000.0) -  100.0
   29)   1     TOTAL TEMPERATURE (FAST RESPONSE) (C)      TTKP      C       = (N/ 1000.0) -  100.0
   30)   1     AMBIENT TEMPERATURE (ROSEMOUNT) (C)        ATW       C       = (N/ 1000.0) -  100.0
   31)   1     AMBIENT TEMPERATURE (REVERSE-FLOW) (C)     ATRF      C       = (N/ 1000.0) -  100.0
   32)   1     AMBIENT TEMPERATURE (FAST RESPONSE) (C)    ATKP      C       = (N/ 1000.0) -  100.0
   33)   1     RADIOMETRIC SURFACE TEMP (PRT-5) (C)       PRT5      C       = (N/ 1000.0) -  100.0
   34)   1     DEW/FROSTPOINT TEMP (THERMOELEC) (C)       DP        C       = (N/ 1000.0) -  100.0
   35)   1     DEWPOINT TEMPERATURE (THERMOELEC) (C)      DPC       C       = (N/ 1000.0) -  100.0
   36)   1     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)      RHOTD     G/M3    = (N/ 1000.0) -  100.0
   37)   1     AIRCRAFT TRUE AIRSPEED (WING) (M/S)        TASW      M/S     = (N/ 1000.0) -  100.0
   38)   1     AIRCRAFT TRUE AIRSPEED (GUST) (M/S)        TASG      M/S     = (N/ 1000.0) -  100.0
   39)   1     VERTICAL DIFF. PRESR (GUST PROBE) (MB)     ADIF      MB      = (N/ 1000.0) -  100.0
   40)   1     ATTACK ANGLE (ROSEMOUNT) (DEG)             ATTACK    DEG     = (N/ 1000.0) -  100.0
   41)   1     HORIZONTAL DIFF. PRESR (GUST PROBE) (MB)   BDIF      MB      = (N/ 1000.0) -  100.0
   42)   1     SIDESLIP ANGLE (ROSEMOUNT) (DEG)           SSLIP     DEG     = (N/ 1000.0) -  100.0
   43)   1     WIND VECTOR EAST GUST COMPONENT (M/S)      UI        M/S     = (N/ 1000.0) -  200.0
   44)   1     WIND VECTOR NORTH GUST COMPONENT (M/S)     VI        M/S     = (N/ 1000.0) -  200.0
   45)   1     WIND VECTOR VERTICAL GUST COMP (H) (M/S)   WI        M/S     = (N/ 1000.0) -  100.0
   46)   1     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)   UX        M/S     = (N/ 1000.0) -  200.0
   47)   1     WIND VECTOR LATERAL GUST COMPONENT (M/S)   VY        M/S     = (N/ 1000.0) -  200.0
   48)   1     HORIZONTAL WIND DIRECTION (DEG)            WDRCTN    DEG     = (N/ 1000.0) -  100.0
   49)   1     HORIZONTAL WIND SPEED (M/S)                WSPD      M/S     = (N/ 1000.0) -  100.0
   50)   1     WIND VECTOR EAST COMPONENT (M/S)           UI1       M/S     = (N/ 1000.0) -  200.0
   51)   1     WIND VECTOR NORTH COMPONENT (M/S)          VI1       M/S     = (N/ 1000.0) -  200.0
   52)   1     WIND VECTOR VERTICAL GUST COMP (L) (M/S)   WI1       M/S     = (N/ 1000.0) -  100.0
   53)   1     WIND VECTOR LNGTDNL COMPONENT (M/S)        UX1       M/S     = (N/ 1000.0) -  200.0
   54)   1     WIND VECTOR LATERAL COMPONENT (M/S)        VY1       M/S     = (N/ 1000.0) -  200.0
   55)   1     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
   56)   1     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
   57)   1     DISTANCE EAST OF START (KM)                DEI       KM      = (N/  100.0) - 5000.0
   58)   1     DISTANCE NORTH OF START (KM)               DNI       KM      = (N/  100.0) - 5000.0
   59)   1     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   60)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
   61)   1     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
   62)   1     DME AIRCRAFT-TO-STATION RANGE (NMI)        DMERNG    NMI     = (N/ 1000.0) -  100.0
   63)   1     ENVIRONMENT 1 RANGE (VDC)                  ENV1R     VDC     = (N/ 1000.0) -  100.0
   64)   1     ENVIRONMENT 1 OUTPUT (VDC)                 ENV1O     VDC     = (N/ 1000.0) -  100.0
   65)   1     ENVIRONMENT 1 CONCENTRATION (N/CM3)        ENV1C     N/CM3   = (N/   10.0) -    0.0
   66)   1     VERTICAL AIR VELOCITY (CSD EQNS.) (M/S)    VAVCSD    M/S     = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  646-01  SEA SALT NUCLEI 12JAN79 14/31/30
 THIS FILE IS ALL OR PART OF THE TIME PERIOD 14        31        30         TO   17        13         0
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                           77 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                        64064 BITS PER PHYSICAL HEADER RECORD
           DATA FILE --  1320 BITS PER LOGICAL DATA RECORD
                           22 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        29040 BITS PER PHYSICAL DATA RECORD