Effects of bottom-structure flexibility on water landing loads of Apollo spacecraft models /

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Bibliographic Details
Author / Creator:	Stubbs, Sandy M., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, March 1969.
Description:	1 online resource (30 pages) : illustrations.
Language:	English
Series:	NASA technical note ; NASA TN D-5108 NASA technical note ; D-5108.
Subject:	Space vehicles -- Landing. Impact. Shielding (Heat) -- Materials -- Testing. Materials -- Dynamic testing. Impact. Materials -- Dynamic testing. Shielding (Heat) -- Materials -- Testing. Space vehicles -- Landing.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12670435

Hidden Bibliographic Details
Other authors / contributors:	Hathaway, Melvin E., author. United States. National Aeronautics and Space Administration, issuing body. Langley Research Center.
Notes:	"March 1969." Includes bibliographical references (page 11). Description based on online resource, PDF version; title from title page (NASA, viewed on Oct. 29, 2020).
Other form:	Print version: Stubbs, Sandy M. Effects of bottom-structure flexibility of water landing loads of Apollo spacecraft models
GPO item no.:	0830-H-13 (online)
Govt.docs classification:	NAS 1.14:D-5108

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