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Attitude of a spinning rocket under thrust with statistically varied error sources.Motion equations of spin stabilized rocket under thrust with jet damping, variable mass and momentum effects and all angular disturbances
Document ID
19680046245
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bullard, C. W.
Papis, T.
Date Acquired
August 4, 2013
Publication Date
May 1, 1968
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 67-536
Report Number: AIAA PAPER 67-536
Meeting Information
Meeting: GUIDANCE, CONTROL AND FLIGHT DYNAMICS CONFERENCE
Location: HUNTSVILLE, AL
Start Date: August 14, 1967
End Date: August 16, 1967
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A27217
Funding Number(s)
CONTRACT_GRANT: NAS7-380
Distribution Limits
Public
Copyright
Other

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