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Design, development, fabrication, test and delivery of electrothermal engine systems Semiannual report, Dec. 1965 - Jun. 1966Ammonia fueled resistojet thrustor system for three-axis attitude control and two-direction station-keeping of stable platform type satellite
Document ID
19670006348
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
John, R. R. (Avco Corp. Wilmington, MA, United States)
Date Acquired
August 3, 2013
Publication Date
December 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AVSSD-0362-66-CR
NASA-CR-72104
Report Number: AVSSD-0362-66-CR
Report Number: NASA-CR-72104
Accession Number
67N15677
Funding Number(s)
CONTRACT_GRANT: NAS3-7934
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPULSION SYSTEM
SATELLITE CONTROL
RESISTOJET ENGINE
ATTITUDE CONTROL
ELECTROTHERMAL ENGINE
THRUSTOR

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