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Conducting the NASP ground test programThe National Aero-Space Plane (NASP) program has recently entered a new phase of the program known as Phase 2D. During this period, five aerospace companies and the Government have formed a National Team. This team has focused on developing a single experimental (X-30) vehicle design and are pursuing a technology validation and demonstration program to prove out the design concepts and design tools. This paper presents an overview of the Phase 2D round testing being conducted to validate the X-30 design and to demonstrate the critical technologies needed to build and fly a research vehicle during Phase 3 of the program. The Phase 2D exit criteria are discussed to identify how they provide top-level guidance for developing the ground test program. An overview of major test facility modifications being performed in support of the test program is also presented. Emphasis is placed on propulsion and structures testing since these are felt to be the primary areas requiring technologies beyond the current state-of-the-art. Also discussed is the use of uncertainty analysis as a method to account for uncertainties in test data. In addition, this paper addresses the use of these uncertainties to develop qualitative indicators of how well the design and technology developed during Phase 2 have matured.
Document ID
19920035196
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
William Sullivan
(Wright-Patterson Air Force Base Wright-Patterson AFB, Ohio, United States)
Date Acquired
August 15, 2013
Publication Date
December 3, 1991
Publication Information
Publication: 3rd International Aerospace Planes Conference
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Astronautics (General)
Report/Patent Number
AIAA-91-5029
Report Number: AIAA PAPER 91-5029
Meeting Information
Meeting: AIAA 3rd International Aerospace Planes Conference
Location: Orlando, FL
Country: US
Start Date: December 3, 1991
End Date: December 5, 1991
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
92A17820
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Airframes
Wind tunnel tests
Defense Advanced Research Projects Agencies
National Aeronautics and Space Administration
Thermal protection system
Design technology
Propulsion system
Hypersonic flight
Hypersonic vehicles
Data analysis
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