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Recommendations for Safe Separation Distances from the Kennedy Space Center (KSC) Vehicle Assembly Building (VAB) Using a Heat-Flux-Based Analytical A
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (08/21/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
The NASA Engineering and Safety Center (NESC) was requested to provide computational modeling to support the establishment of a safe separation distance surrounding the Kennedy Space Center (KSC) Vehicle Assembly Building (VAB). The two major objectives of the study were 1) establish a methodology based on thermal flux to determine safe separation distances from the Kennedy Space Center's (KSC's) Vehicle Assembly Building (VAB) with large numbers of solid propellant boosters containing hazard division 1.3 classification propellants, in case of inadvertent ignition; and 2) apply this methodology to the consideration of housing eight 5-segment solid propellant boosters in the VAB. The results of the study are contained in this report. Cragg, Clinton H. and Bowman, Howard and Wilson, John E. Langley Research Center NASA/TM-2011-217071, NESC-RP-06-061, L-20003, NF1676L-12397 WBS 869021.05.07.04.99
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Product Details
ISBN-13:
9798676642921
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
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Page Count:
96
Carton Quantity:
42
Product Dimensions:
8.50 x 0.20 x 11.02 inches
Weight:
0.54 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
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publisher marketing
The NASA Engineering and Safety Center (NESC) was requested to provide computational modeling to support the establishment of a safe separation distance surrounding the Kennedy Space Center (KSC) Vehicle Assembly Building (VAB). The two major objectives of the study were 1) establish a methodology based on thermal flux to determine safe separation distances from the Kennedy Space Center's (KSC's) Vehicle Assembly Building (VAB) with large numbers of solid propellant boosters containing hazard division 1.3 classification propellants, in case of inadvertent ignition; and 2) apply this methodology to the consideration of housing eight 5-segment solid propellant boosters in the VAB. The results of the study are contained in this report. Cragg, Clinton H. and Bowman, Howard and Wilson, John E. Langley Research Center NASA/TM-2011-217071, NESC-RP-06-061, L-20003, NF1676L-12397 WBS 869021.05.07.04.99
Show More