Example Input File (ascii format)


HEADER OPTIONS DATA

C                          <<< SIRTF THERMAL MATH MODEL >>>
C                                Mid 80s Configuration

   SOLRTN  = SSITER      $ Steady State solution
   SUMMARY = ON          $ Print data block summaries
   UID    =  SI

HEADER CONTROL DATA

  SIGMA  =  .56700E-08   $ Stephan-Boltzmann
  ABSZRO =      0.000    $ Absolute temperature

c MLI Blankets: effective emissivity ,area (sqcm), and thickness (cm)
  E_outer = .00081 , A_outer = 5.617E+05, T_outer = 8.  $ Outer MLI OS to OVCS
  E_mid   = .0019  , A_mid   = 5.368E+05, T_mid   = 4.  $ OVCS to MVCS
  E_inner = .0056  , A_inner = 5.186E+05, T_inner = 3.  $ MVCS to IVCS
  E_last  = .01361 , A_last  = 3.969E+05                $ IVCS to MCT
                     A_fb    = 2.077E+04                $ area of fwd baffle

  C_mli = 1.5E-06       $ MLI conductivity mw/cm-K


HEADER NODE DATA

       1,   10.000,  1.00 $  Clevis
     117,   10.000,  1.00 $  Hot MIC
     118,   10.000,  1.00 $  Cold MIC
     220,   10.000,  1.00 $  Forward Baffle
     260,   10.000,  1.00 $  Secondary Mirror
     261,   10.000,  1.00 $  Chopper Motor and Housing
     280,   10.000,  1.00 $  FGS                                    
     301,   10.000,  1.00 $  IVCS                                   
     401,   10.000,  1.00 $  MVCS                                   
     501,   10.000,  1.00 $  OVCS                                   
     621,   10.000,  1.00 $  Strap, outer
     622,   10.000,  1.00 $  Strap, mid
     623,    0.010,  1.00 $  Strap, inner
    -800,    1.700,  1.00 $  MCT (main cryo tank)
    -900,  200.000,  1.00 $  Outer Shell

HEADER CONDUCTOR DATA

c           internal radiation
     -1001,  900,  501, 0.372E+02   ,-1002,  220,  261, 0.1362E+02
     -1003,  220,  800, 0.179E+01   ,-1004,  220,  800, 0.588E+04

C          MLI   ( area(sqcm) * e )

     -1005, 900, 501, A_outer * E_outer ,-1006, 501, 401, A_mid * E_mid
     -1007, 401, 301, A_inner * E_inner ,-1008, 301, 220, A_fb  * E_last
     -1009, 301, 800, A_last  * E_last

      2001, 118, 800, 25.                               $ Baseplate to Cold MIC
      2002,   1, 900, 25.                               $ OS to clevis
      2003, 117, 800, 15.   , 2004, 117, 800, .207      $ Hot MIC
      2005, 260, 261, .15   , 2006, 261, 800, 15.0      $ Sec mirror Assy

      2007,  220,  301, 10.0                            $ FB support, Fiberglas
      2008,  280,  501, 10.0                            $ FGS sunk to OVCS

      2009, 621, 501, 100.,   2010, 622, 401, 100.      $ Straps to VCS
      2011, 623, 301, 100.                              $ Straps to VCS

      2012, 900, 301, .235,   2013, 301, 800, .00267    $ fill line

      2014, 900, 501, 2.48,   2015, 501, 401, 8.87      $ wires
      2016, 401, 301, 5.53,   2017, 301, 800, .418      $ wires

      2018, 900, 501, C_mli * A_outer / T_outer         $ MLI conductance
      2019, 501, 401, C_mli * A_mid   / T_mid           $ MLI conductance
      2020, 401, 301, C_mli * A_inner / T_inner         $ MLI conductance

c            Flow conductors as a funtion of heat load on node 998 (helium)
c            Hv(helium)=23000.
     FLQ   3001, -800,  261, 500, 1./23000., 800 $
     FLQ   3002, -261,  117, 500, 1./23000., 800 $
     FLQ   3003, -117,  220, 500, 1./23000., 800 $
     FLQ   3004, -220,  301, 500, 1./23000., 800 $
     FLQ   3005, -301,  401, 500, 1./23000., 800 $
     FLQ   3006, -401,  501, 500, 1./23000., 800 $

c             Strap conduction a function of temperature
     SIV  4001,     1,   621,   1, 0.123E+01 $  STRAPS L=30 cm AREA=36.8 sqcm
     SIV  4002,   621,   622,   1, 0.613E+01 $  STRAPS L=6.0
     SIV  4003,   622,   623,   1, 0.123E+02 $  STARPS L=3.0
     SIV  4004,   623,   800,   1, 0.968E+00 $  STRAPS L=38.

     SIV  4005,   280,   800,   2, 0.242E-01 $  FGS mounting (fiberglas tube)


HEADER ARRAY DATA

     500   $ Cp(helium)
       0., 5200.,   300.,5200.,  END


c     Thermal Conductivity of Straps
               1

c             T          k
c            (K)      (mw/cm-K)
c          -----------------------
             4.000,     0.584
             5.000,     0.814
             6.000,     .9900
             8.000,     1.240
            10.000,     1.400
            15.000,     1.650
            30.000,     2.150
            40.000,     2.480
            50.000,     2.850
            60.000,     3.180
            80.000,     3.880
           100.000,     4.540
           150.000,     6.000
           200.000,     7.190
           300.000,     8.900,  END

C
C   THERMAL CONDUCTIVITY OF G-10CR
C
               2
C
C             T          k
C            (K)     (mW/cm-K)
C           -----    ---------
              0.0,      0.000
              4.0,      0.881
              6.0,      1.080
              8.0,      1.260
             10.0,      1.410
             15.0,      1.730
             20.0,      2.010
             25.0,      2.250
             30.0,      2.470
             35.0,      2.680
             40.0,      2.870
             50.0,      3.220
             60.0,      3.550
             70.0,      3.820
             76.0,      4.000
             80.0,      4.100
             90.0,      4.360
            100.0,      4.600
            120.0,      5.050
            140.0,      5.470
            160.0,      5.870
            180.0,      6.230
            200.0,      6.580
            250.0,      7.370
            300.0,      8.100, END

HEADER SOURCE DATA

C   Constant Heat Sources   (mw)

       117,   150.000      $ hot MIC
       118,    50.000      $ cold MIC
       261,    30.000      $ chopper motor
       280,    50.000      $ FGS
       220,    80.000      $ Aperature heating

END OF DATA


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