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
Aerodynamic stability characteristics of the Apollo launch escape vehicleAerodynamic stability of Apollo launch escape vehicle
Document ID
19670020797
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hondros, J. G. (NASA Manned Spacecraft Center Langley Station, VA, United States)
Moseley, W. C., Jr. (NASA Manned Spacecraft Center Langley Station, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1967
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-3964
Report Number: NASA-TN-D-3964
Accession Number
67N30126
Funding Number(s)
CONTRACT_GRANT: 914-50-10-03-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LAUNCH ESCAPE SYSTEM /LES/
AERODYNAMIC STABILITY
APOLLO SPACECRAFT

Related Records

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