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Solid-propellant motors for high-incremental velocity low-acceleration maneuvers in spaceLow thrust long burning solid rocket propellant motor for orbit insertion maneuvers, discussing design, static tests, nozzle composition, igniter and performance
Document ID
19710061319
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shafer, J. I.
Date Acquired
August 6, 2013
Publication Date
September 1, 1971
Subject Category
Propulsion Systems
Meeting Information
Meeting: INTERNATIONAL ASTRONAUTICAL CONGRESS
Location: BRUSSELS
Country: BELGIUM
Start Date: September 20, 1971
End Date: September 25, 1971
Sponsors: INTERNATIONAL ASTRONAUTICAL FEDERATION
Accession Number
71A42016
Distribution Limits
Public
Copyright
Other

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