Actions for Landing characteristics of the Apollo spacecraft with deployed-heat-shield impact attenuation systems

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Landing characteristics of the Apollo spacecraft with deployed-heat-shield impact attenuation systems

Author
Stubbs, S. M.
Published
Jan 1, 1966.
Physical Description
1 electronic document
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Impact acceleration and landing system characteristics of Apollo spacecraft command module configurations with deployed heat shield
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19660005612.
Accession ID: 66N14901.
NASA-TN-D-3059.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15958888