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Application of combined high- and low-thrust propulsion systems to planetary missions.Vehicle mass requirements for optimal high and low thrust propulsion systems for manned and unmanned planetary missions
Document ID
19670058396
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ragsac, R. V.
Date Acquired
August 3, 2013
Publication Date
April 1, 1967
Publication Information
Publication: ASTRONAUTICA ACTA
Subject Category
Space Vehicles
Accession Number
67A37125
Funding Number(s)
CONTRACT_GRANT: NAS8-11309
Distribution Limits
Public
Copyright
Other
Keywords
MISSION PLANNING
THRUST POWER
PLANETARY SPACE FLIGHT
MASS RATIO

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