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Configuration development study of the X-24C hypersonic research airplane, phase 3The conclusion evolved from the three phased study on the configuration development of the X-24C Hypersonic Research Airplane makes it evident that it is practical to design and build the high performance National Hypersonic Flight Research Facility airplane with today's state of the art within the cost and operational constraints established by NASA. The vehicle launched at 31.75 Mg from the B-52 can cruise for 40 seconds at Mach 6.78 on scramjets. Without scramjets it can approach Mach 8 with a 453.6 Kg payload or do 70 seconds of cruise at Mach 6 with a 2.27 Mg payload. Reduction in cost is possible with a vehicle scaled to a lesser mass and capability.
Document ID
19790008669
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Combs, H. G.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-145103
Report Number: NASA-CR-145103
Accession Number
79N16840
Funding Number(s)
CONTRACT_GRANT: NAS1-14222
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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