Catalog Record: Water pressures and accelerations during landing of a dynamic model of the Apollo spacecraft with a deployed-heat-shield impact-attenuation system | HathiTrust Digital Library

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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.

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Main Author: Stubbs, Sandy M.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; [1968]
Subjects: Materials > Materials / Dynamic testing.
Shielding (Heat) > Shielding (Heat) / Materials > Shielding (Heat) / Materials / Testing.
Impact.
Space vehicles > Space vehicles / Landing.
Note: Prepared at Langley Research Center.
"Technical film supplement L-980 available on request."
"March 1968"--Cover.
Physical Description: 44 p. : ill. ; 27 cm.
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