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Kennedy Space Center (KSC) Launch Complex 39 (LC-39) Gaseous Hydrogen (GH2) Vent Arm Behavior Prediction Model Review Technical Assessment Report
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (07/30/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
The NESC Assessment Team reviewed a computer simulation of the LC-39 External Tank (ET) GH2 Vent Umbilical system developed by United Space Alliance (USA) for the Space Shuttle Program (SSP) and designated KSC Analytical Tool ID 451 (KSC AT-451). The team verified that the vent arm kinematics were correctly modeled, but noted that there were relevant system sensitivities. Also, the structural stiffness used in the math model varied somewhat from the analytic calculations. Results of the NESC assessment were communicated to the model developers. Wilson, Timmy R. and Beech, Geoffrey and Johnston, Ian Kennedy Space Center; Langley Research Center; Marshall Space Flight Center NASA/TM-2009-215570, NESC-RP-05-114/05-013-E, L-19605, LF99-8397 WBS 510505.01.07.01.06 EXTERNAL TANKS; SPACE SHUTTLES; STIFFNESS; VENTS; KINEMATICS; COMPUTERIZED SIMULATION; ANALYSIS (MATHEMATICS); MATHEMATICAL MODELS; CAPE KENNEDY LAUNCH COMPLEX; HYDROGEN
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Product Format
Product Details
ISBN-13:
9798670917254
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
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Page Count:
38
Carton Quantity:
108
Product Dimensions:
8.50 x 0.08 x 11.02 inches
Weight:
0.25 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
Descriptions, Reviews, Etc.
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The NESC Assessment Team reviewed a computer simulation of the LC-39 External Tank (ET) GH2 Vent Umbilical system developed by United Space Alliance (USA) for the Space Shuttle Program (SSP) and designated KSC Analytical Tool ID 451 (KSC AT-451). The team verified that the vent arm kinematics were correctly modeled, but noted that there were relevant system sensitivities. Also, the structural stiffness used in the math model varied somewhat from the analytic calculations. Results of the NESC assessment were communicated to the model developers. Wilson, Timmy R. and Beech, Geoffrey and Johnston, Ian Kennedy Space Center; Langley Research Center; Marshall Space Flight Center NASA/TM-2009-215570, NESC-RP-05-114/05-013-E, L-19605, LF99-8397 WBS 510505.01.07.01.06 EXTERNAL TANKS; SPACE SHUTTLES; STIFFNESS; VENTS; KINEMATICS; COMPUTERIZED SIMULATION; ANALYSIS (MATHEMATICS); MATHEMATICAL MODELS; CAPE KENNEDY LAUNCH COMPLEX; HYDROGEN
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