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High altitude reconnaissance aircraft designA Universities Space Research Association (USRA) sponsored (undergraduate) study is presented on the feasibility and design of a high altitude reconnaissance/research aircraft. The aircraft mission was to carry 1,000-3,000 lb of atmospheric pollutant monitoring equipment for 1-5 hr at an altitude of 100,000-130,000 ft. Three configurations subject to the same mission requirements were studied in detail. The three designs analyzed were the tandem-wing-twin-boom, joined wing, and conventional twin-boom configurations. The performance of the three proposed configurations is presented and shows that high altitude flight is possible with current technology. Different possible propulsion systems were investigated and suggestions are made for further investigation and better optimization of the designs.
Document ID
19940004546
Document Type
Conference Paper
Authors
Poladian, D.
(California State Polytechnic Univ. Pomona, CA, United States)
Reinhard, D. J.
(California State Polytechnic Univ. Pomona, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1989
Publication Information
Publication: USRA, NASA(USRA University Advanced Design Program Fifth Annual Summer Conference
Subject Category
Aircraft Design, Testing And Performance
Accession Number
94N71301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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