NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Mechanical Impact System Design for Advanced Spacecraft /MISDAS/. Phase I - Design Concept SelectionMechanical impact system for earth landing of Apollo command module
Document ID
19670005559
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bernstein, A. I. (North American Aviation, Inc. Downey, CA, United States)
Date Acquired
August 3, 2013
Publication Date
September 20, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-80968
SID-65-1205
Report Number: NASA-CR-80968
Report Number: SID-65-1205
Accession Number
67N14888
Funding Number(s)
CONTRACT_GRANT: NAS9-4915
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMMAND MODULE
REENTRY VEHICLE
APOLLO SPACECRAFT

Related Records

There are no records associated with this record.
No Preview Available