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Manx: Close air support aircraft preliminary designThe Manx is a twin engine, twin tailed, single seat close air support design proposal for the 1991 Team Student Design Competition. It blends advanced technologies into a lightweight, high performance design with the following features: High sensitivity (rugged, easily maintained, with night/adverse weather capability); Highly maneuverable (negative static margin, forward swept wing, canard, and advanced avionics result in enhanced aircraft agility); and Highly versatile (design flexibility allows the Manx to contribute to a truly integrated ground team capable of rapid deployment from forward sites).
Document ID
19920012322
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Amy, Annie
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Crone, David
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Hendrickson, Heidi
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Willis, Randy
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Silva, Vince
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Date Acquired
September 6, 2013
Publication Date
November 25, 1991
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-189992
NAS 1.26:189992
Report Number: NASA-CR-189992
Report Number: NAS 1.26:189992
Accession Number
92N21565
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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