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Aeroassisted orbit transfer window opens on missionsStudies of aeroassisted spacecraft orbit transfer conducted over the last two decades have produced an extensive literature and a well developed technology base, which suggest the obtainability of substantial performance improvements over all-propulsive spacecraft maneuvers. In such cases as that of multipass aerobraking, in which the vehicle is transferred from its approach velocity to a highly elliptic orbit about the planet by means of a rocket burn, followed by the circularization of the orbit through many high altitude atmospheric passes, the technology appears to be ready for application. In most other areas of aeroassisted orbit transfer, further work is required to reduce design risks to acceptable levels.
Document ID
19840028104
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Walberg, G. D.
(NASA Langley Research Center Space Systems Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
November 1, 1983
Publication Information
Publication: Astronautics and Aeronautics
Volume: 21
ISSN: 0004-6213
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ISSN: 0004-6213
Accession Number
84A10891
Distribution Limits
Public
Copyright
Other

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