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Conceptual design of a next-generation, fully reusable manned launch systemThe conceptual design of a rocket-powered, two-stage fully reusable launch vehicle has been performed as a part of the Advanced Manned Launch System (AMLS) study at the NASA Langley Research Center. The main goals of the AMLS study are to provide routine, low-cost manned access to space. Technologies and system approaches have been studied that would contribute to significant reductions in operating costs relative to current systems. System and operational characteristics of the two-stage fully reusable vehicle are presented, and the various tools and methods used in the design process are summarized. The results of a series of trade studies performed to examine the effect of varying major vehicle parameters on the reference two-stage fully reusable vehicle are also summarized.
Document ID
19910034725
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stanley, Douglas O.
(NASA Langley Research Center Hampton, VA, United States)
Talay, Theodore A.
(NASA Langley Research Center Hampton, VA, United States)
Lepsch, Roger A.
(NASA Langley Research Center Hampton, VA, United States)
Morris, W. Douglas
(NASA Langley Research Center Hampton, VA, United States)
Wurster, Kathryn E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 91-0537
Report Number: AIAA PAPER 91-0537
Accession Number
91A19348
Distribution Limits
Public
Copyright
Other

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