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High performance dash on warning air mobile, missile systemAn aircraft-missile system which performs a high acceleration takeoff followed by a supersonic dash to a 'safe' distance from the launch site is presented. Topics considered are: (1) technological feasibility to the dash on warning concept; (2) aircraft and boost trajectory requirements; and (3) partial cost estimates for a fleet of aircraft which provide 200 missiles on airborne alert. Various aircraft boost propulsion systems were studied such as an unstaged cryogenic rocket, an unstaged storable liquid, and a solid rocket staged system. Various wing planforms were also studied. Vehicle gross weights are given. The results indicate that the dash on warning concept will meet expected performance criteria, and can be implemented using existing technology, such as all-aluminum aircraft and existing high-bypass-ratio turbofan engines.
Document ID
19760003000
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Levin, A. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Castellano, C. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Hague, D. S.
(Aerophysics Res. Corp. Bellevue, Wash., United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
A-6260
NASA-TM-X-62479
Accession Number
76N10088
Funding Number(s)
PROJECT: RTOP 791-40-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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