rr052-pre-launch-thermal-analysis-of-two-stage-reusable-launch-vehicle's Introduction

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Pre-Launch Thermal Analysis of Two-Stage Reusable Launch Vehicle:

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Pre-Launch Thermal Analysis of Two-Stage Reusable Launch Vehicle using SindaG.

I. Operation: "./run_sinda180a.bat"

II. SindaG Input File: "./k1_pre_launch_f.sin"

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START: Input File: "k1_pre_launch_f.sin"
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  This model contains all of the physical connection that were
  modeled in the Thermal Analysis.

  The model units are Metric:
  Length:		Meters
  Mass:		Kilograms
  Time:		Seconds
  Temperature:	deg C
  
  
  A brief description of the Node IDs is given below

  NAME                               First Node   Last Node
  ---------------------------------  ----------   ---------
  OV STRUCTURES LRU                        1        1735
  OV LOX TANK                           2001        2197
  OV PROPULSION LRU                     2201        2665
  OV LANDING LRU                        2701        2749
  OV ELECTRONICS LRU                    2801        2941
  OV TPS                                3001        7066
  ADD'L ARITHMETIC NODES                8001        8137
  OV OPPENHEIM ELEMENTS (RADIATION)    40001       47066
  OV OPPENHEIM ELEMENTS (RADIATION)    60073       42938

  LAP STRUCTURES LRU                    10001       11356
  LAP LOX TANK                          11501       11752
  LAP RP TANK                           11801       12064
  LAP LANDING LRU                       12101       12167
  LAP PROPULSION LRU                    12201       12756
  LAP PROPULSION LRU - AVIONCS          12801       12857
  LAP ELECTRONICS LRU                   12901       13011
  LAP TPS                               13101       17126
  ADD'L ARITHMETIC NODES                18001       18410
  ADD'L ARITHMETIC NODES (BOOTS)        18411       18538
  LAP OPPENHEIM ELEMENTS (RADIATION)    50001       57126
  LAP OPPENHEIM ELEMENTS (RADIATION)    70001       73008
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END: Input File: "k1_pre_launch_f.sin"
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