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Technology challenges for the National Aero-Space PlaneThe National Aerospace Plane (NASP) will require an exceptionally high degree of integration between propulsion and aerodynamic configuration, in order to achieve the requisite specific impulse and low structural weight. This is to be achieved through the use of forebody shock compression and afterbody exhaust expansion. Attention is presently given to the materials and structural concepts required for the realization of these NASP airframe functions, in view of the exceptionally high aerothermodynamic loads that will be experienced at hypersonic speeds. Active cooling will have to be used in certain critical airframe and propulsion components. CFD characterizations of these processes must be carefully developed and fully validated.
Document ID
19880028711
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Piland, William M.
(NASA National Aero-Space Plane Program Management Office Washington, DC, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1987
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 87-205
Accession Number
88A15938
Distribution Limits
Public
Copyright
Other

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