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Heavy-lift launch vehicle propulsion considerationsInformation on heavy-lift launch vehicle (HLLV) propulsion is given in viewgraph form. The objective was to investigate Earth to orbit options which minimize on-orbit operations and impacts to Space Station Freedom, have a reasonable capability to support Mars missions, and minimize mass in low Earth orbit. Potential synergism with the Space Transportation System is considered. Launch vehicle sizing results, HLLV thrust requirements, and propulsion system reliability are covered.
Document ID
19910018922
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ordway, Wayne L. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: NASA, Washington, Space Transportation Propulsion Technology Symposium. Volume 3: Panel Session Summaries and Presentations
Subject Category
Spacecraft Propulsion And Power
Accession Number
91N28236
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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