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Manned Venus FlybyThis study is one of several being conducted at Bellcomm and in Manned Space Flight whose purpose is to give guidance to the Apollo Applications Program's technical objectives by focusing on a longer range goal. The assumed mission in this case is a three-man flyby of Venus launched in November, 1973 on a single standard Saturn V. The selected flight configuration includes a Command and Service Module similar in some respects to Apollo, an Environmental Support Module which occupies the adapter area and a spent S-IVB stage which is utilized for habitable volume and structural support of a solar cell electrical power system. The total injected weight, 106,775 lbs., is within the capability of a single Saturn V of the early 1970's. The study is focused on the selection of subsystem technologies appropriate to long duration flight. The conclusions are reported in terms of the technical characteristics to be achieved as part of the Apollo Applications Program's long duration objectives.
Document ID
19790072165
Document Type
Contractor Report (CR)
Authors
Feldman, M. S. (Bellcomm, Inc. Washington, DC, United States)
Ferrara, L. A. (Bellcomm, Inc. Washington, DC, United States)
Havenstein, P. L. (Bellcomm, Inc. Washington, DC, United States)
Volonte, J. E. (Bellcomm, Inc. Washington, DC, United States)
Whipple, P. H. (Bellcomm, Inc. Washington, DC, United States)
Date Acquired
August 9, 2013
Publication Date
February 1, 1967
Subject Category
ASTRONAUTICS (GENERAL)
Report/Patent Number
TR-67-600-1-1
NASA-CR-114025
Funding Number(s)
CONTRACT_GRANT: NASW-417
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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