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
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Space Shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...
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Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster pro...
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NASA is developing launch vehicles to support missions to Low Earth Orbit (LEO), the moon and deep s...
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster pro...
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
NASA is developing launch vehicles to support missions to Low Earth Orbit (LEO), the moon and deep s...
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...
Numerical analysis of techniques for separating space shuttles by separation rockets, spring loaded ...
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster pro...
Mr. Steve Rickman, NASA Technical Fellow for Passive Thermal, proposed a pathfinder study to develop...
This report documents a parametric sizing study performed to develop a program strategy for research...
A trade study and litera ture survey of refractory materials (fi rebrick. refractory concrete. and s...
Space Shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...
As the NASA center responsible for assembly, checkout, servicing, launch, recovery, and operational ...
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster pro...
Heat transfer, altitude performance, and combustion efficiency evaluated in study of space storable ...
Since the loss of Columbia on February 1, 2003, the Space Shuttle Program (SSP) has significantly im...
NASA is developing launch vehicles to support missions to Low Earth Orbit (LEO), the moon and deep s...
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster pro...
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas