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Pulse motor for spacecraft attitude control.Multipulse thruster module design and development tests for spacecraft attitude control, noting micropulse solid propellant rocket motor
Document ID
19690033773
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blackwood, D.
Suddeth, D.
Date Acquired
August 5, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: AMERICAN ASTRONAUTICAL SOCIETY,
Subject Category
Auxiliary Systems
Accession Number
69A11762
Distribution Limits
Public
Copyright
Other

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