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Data for vehicle design for earth orbit to mars orbit and return.Payload and speed requirements of an earth orbit to mars orbit and return manned spacecraft, using a nuclear heat exchanger-type propulsion system
Document ID
19640024214
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ruppe, H. O.
Date Acquired
August 2, 2013
Publication Date
January 1, 1963
Subject Category
Structural Mechanics
Accession Number
64A10107
Distribution Limits
Public
Copyright
Other
Keywords
NUCLEAR PROPULSION
PLANETARY EXPLORATION
MANNED SPACE FLIGHT
SPACECRAFT DESIGN

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