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Designing for space - An inertial guidance sensor for lunar orbiter.Inertial reference unit to provide attitude and thrust maneuver measurements for Lunar Orbiter spacecraft
Document ID
19660040239
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Simon, J. M.
Date Acquired
August 3, 2013
Publication Date
January 1, 1965
Subject Category
Navigation
Accession Number
66A19529
Funding Number(s)
CONTRACT_GRANT: NAS1-3800
Distribution Limits
Public
Copyright
Other
Keywords
GUIDANCE SENSOR
INERTIAL REFERENCE SYSTEM
LUNAR ORBIT

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