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Optimal low-thrust takeoff from an orbit about an oblate planetLow thrust vehicle optimal takeoff calculations from orbit about oblate planet, using two variable asymptotic expansion technique
Document ID
19710062340
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jacobson, R. A.
Powers, W. F.
Date Acquired
August 6, 2013
Publication Date
August 1, 1971
Publication Information
Publisher: AMERICAN ASTRONAUTICAL SOCIETY,
Subject Category
Space Sciences
Report/Patent Number
AAS PAPER 71-367
Report Number: AAS PAPER 71-367
Meeting Information
Meeting: ASTRODYNAMICS SPECIALISTS CONFERENCE
Location: FT. LAUDERDALE, FL
Country: US
Start Date: August 17, 1971
End Date: August 19, 1971
Sponsors: AMERICAN ASTRONAUTICAL SOCIETY, AIAA
Accession Number
71A43037
Funding Number(s)
CONTRACT_GRANT: NGR-23-005-329
Distribution Limits
Public
Copyright
Other

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