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Inertial measurement units and pulse torquingInertial measurement unit, pulsed integrating pendulous accelerometer, and coupling data unit of Apollo guidance and control system
Document ID
19660019470
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Miller, J. E.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 3, 2013
Publication Date
June 1, 1965
Subject Category
Navigation
Accession Number
66N28760
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MANNED SPACE FLIGHT
INERTIAL MEASURING UNIT
APOLLO SPACECRAFT
GUIDANCE AND CONTROL
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