A comparison study of a GE-21 variable propulsion system with a Multimode Integrated Propulsion System (MMIPS) was conducted while installed in small M = 2.7 supersonic cruise vehicles with military and business jet possibilities. The 1984 state of the art vehicles were sized to the same transatlantic range, takeoff distance, and sideline noise. The results indicate the MMIPS would result in a heavier vehicle with better subsonic cruise performance. The MMIPS arrangement with one fan engine and two satellite turbojet engines would not be appropriate for a small supersonic business jet because of design integration penalties and lack of redundancy.
Supersonic cruise vehicle research/business jet
1980-03-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Supersonic Cruise Research 1979, part 2
NTRS | 1980
Overview of Supersonic Cruise Propulsion Research
NTIS | 1991
|Supersonic Cruise Research 1979, part 1
NTRS | 1980
Fabrication research for supersonic cruise aircraft
Tema Archiv | 1979
|TIBKAT | 1985
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