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A Mars airplaneAn airplane specifically designed for Mars flight is described, emphasizing its conceivable role as an aerial surveyor for visual imaging, gamma-ray and IR reflectance spectroscopy, studies of atmospheric composition and dynamics, and gravity-field, magnetic-field, and electromagnetic sounding. Possible imaging systems and surveying tasks are considered, along with a plausible mission scenario for a fleet of 12 airplanes, which would be taken to Mars in squadrons of four by three Shuttle/IUS Twin Stage/spacecraft carriers. A basic configuration closely resembling that of a competition glider is examined, and four types of airplane are discussed: hydrazine-powered cruisers and landers and electrically powered cruisers and landers. Attention is given to navigation, guidance, and control avionics, vehicle weight, the use of composite materials for the wing, and flight testing on earth.
Document ID
19790033862
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Clarke, V. C.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Kerem, A.
(Developmental Sciences, Inc. City of Industry, Calif., United States)
Lewis, R.
(Lear Siegler, Inc. Astronics Div., Santa Monica, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: Astronautics and Aeronautics
Volume: 17
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
79A17875
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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