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Air-breathing aerospace plane development essential: Hypersonic propulsion flight testsHypersonic air-breathing propulsion utilizing scramjets can fundamentally change transatmospheric accelerators for low earth-to-orbit and return transportation. The value and limitations of ground tests, of flight tests, and of computations are presented, and scramjet development requirements are discussed. It is proposed that near full-scale hypersonic propulsion flight tests are essential for developing a prototype hypersonic propulsion system and for developing computational-design technology so that it can be used for designing this system. In order to determine how these objectives should be achieved, some lessons learned from past programs are presented. A conceptual two-stage-to-orbit (TSTO) prototype/experimental aerospace plane is recommended as a means of providing access-to-space and for conducting flight tests. A road map for achieving these objectives is also presented.
Document ID
19950008507
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mehta, Unmeel B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Aeronautics (General)
Report/Patent Number
A-95017
NASA-TM-108857
NAS 1.15:108857
Meeting Information
Meeting: European Symposium on Aerothermodynamics for Space Vehicles, ESTEC
Location: Noordwijk
Country: Netherlands
Start Date: November 21, 1994
End Date: November 23, 1994
Accession Number
95N14921
Funding Number(s)
PROJECT: RTOP 505-59-53
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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