Mission/flight systems integration study (M/FSIS)

Author

Schneider, Bernard A.

Author_Institution

Wright-Patterson AFB, OH, USA

fYear

1989

fDate

22-26 May 1989

Firstpage

64

Abstract

The objectives of the two-phase M/FSIS project, spanning fiscal years 1988-91 are to develop functional capability requirements for electronic systems (avionics) needed in mission applications and air vehicles to operate effectively in the year-2010 timeframe; and develop conceptual electronic systems (avionics) functional integration design concepts and associated technology development objectives (road-maps) for satisfying air-vehicle integrated-system requirements. The scope of the 18-month Phase I effort is to develop electronic systems functional capability requirements for a set of seven air vehicles and associated missions, namely fighter, interdictor, stand-off strategic weapons carrier, attacker, airlifter, transatmospheric, and special-operations-forces vertical airlifter. Phase I will also identify the system and enabling technologies to satisfy these requirements

Keywords

aircraft instrumentation; military systems; air vehicles; air-vehicle integrated-system; aircraft instrumentation; airlifter; attacker; fighter; functional integration; interdictor; military systems; mission flight systems integration; road-maps; special-operations-forces vertical airlifter; stand-off strategic weapons carrier; transatmospheric airlifter; Aerospace electronics; Costs; Investments; Laboratories; Military aircraft; Performance analysis; Road vehicles; Technology planning; Variable speed drives; Weapons;

fLanguage

English

Publisher

ieee

Conference_Titel

Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National

Conference_Location

Dayton, OH

Type

conf

DOI

10.1109/NAECON.1989.40193

Filename

40193