NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Touchdown stability studyThree-dimensional parameter effects on dynamic stability of Surveyor vehicle landing system
Document ID
19670006386
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Garba, J. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
October 31, 1966
Subject Category
Space Vehicles
Accession Number
67N15715
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DYNAMIC STABILITY
LANDING SYSTEM
SURVEYOR PROJECT
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available