Water pressures and accelerations during landing of a dynamic model of the Apollo spacecraft with a deployed-heat-shield impact-attenuation system /
by Sandy M. Stubbs.
|Main Author:||Stubbs, Sandy M.|
Washington, D.C. : National Aeronautics and Space Administration ; 
Shielding (Heat) > Shielding (Heat) / Materials > Shielding (Heat) / Materials / Testing.
Space vehicles > Space vehicles / Landing.
Prepared at Langley Research Center.
"Technical film supplement L-980 available on request."
44 p. :
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|Full view||University of Illinois at Urbana-Champaign|