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Reusable Launch Vehicle Technology ProgramIndustry/NASA reusable launch vehicle (RLV) technology program efforts are underway to design, test, and develop technologies and concepts for viable commercial launch systems that also satisfy national needs at acceptable recurring costs. Significant progress has been made in understanding the technical challenges of fully reusable launch systems and the accompanying management and operational approaches for achieving a low cost program. This paper reviews the current status of the RLV technology program including the DC-XA, X-33 and X-34 flight systems and associated technology programs. It addresses the specific technologies being tested that address the technical and operability challenges of reusable launch systems including reusable cryogenic propellant tanks, composite structures, thermal protection systems, improved propulsion and subsystem operability enhancements. The recently concluded DC-XA test program demonstrated some of these technologies in ground and flight test. Contracts were awarded recently for both the X-33 and X-34 flight demonstrator systems. The Orbital Sciences Corporation X-34 flight test vehicle will demonstrate an air-launched reusable vehicle capable of flight to speeds of Mach 8. The Lockheed-Martin X-33 flight test vehicle will expand the test envelope for critical technologies to flight speeds of Mach 15. A propulsion program to test the X-33 linear aerospike rocket engine using a NASA SR-71 high speed aircraft as a test bed is also discussed. The paper also describes the management and operational approaches that address the challenge of new cost effective, reusable launch vehicle systems.
Document ID
19990009876
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Freeman, Delma C., Jr.
(NASA Langley Research Center Hampton, VA United States)
Talay, Theodore A.
(NASA Langley Research Center Hampton, VA United States)
Austin, R. Eugene
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1997
Publication Information
Publication: Acta Astronautica
Publisher: Pergamon
Volume: 41
Issue: 11
ISSN: 0094-5765
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
IAF-96-V.4.01
Distribution Limits
Public
Copyright
Other

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