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Optimization of ''ephemeridal'' parameters for minimum propellant requirements on multiplanet roundtrip swingby-stopover missions.Ephemeridal parameter optimization for minimum propellant requirements for round trip swingby- stopover multiplanet mission
Document ID
19680057758
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mead, C. W.
Young, A. C.
Date Acquired
August 4, 2013
Publication Date
September 1, 1968
Publication Information
Publisher: AMERICAN ASTRONAUTICAL SOCIETY,
Subject Category
Space Sciences
Report/Patent Number
AAS PAPER 68-147
Report Number: AAS PAPER 68-147
Meeting Information
Meeting: ASTRODYNAMICS SPECIALIST CONFERENCE
Location: JACKSON, WY
Country: US
Start Date: September 3, 1968
End Date: September 5, 1968
Sponsors: AMERICAN ASTRONAUTICAL SOCIETY, AIAA
Accession Number
68A38730
Distribution Limits
Public
Copyright
Other

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