In this study, new technology engines were defined in two power classes: a 200 hp class, for a light, 4-place personal aircraft, and a 1500 pound thrust class for a twin-engined, 6 place business jet type aircraft. The engines were evaluated for retrofitting suitable current production aircraft for comparison to the existing engines. The engines were evaluated for performance using a typical mission for each aircraft, as well as a variant mission to further appraise performance.Issues of cost, safety, maintenance, and reliability were also addressed. Manufacturing plans were then constructed.
Advanced Propulsion System Studies for General Aviation Aircraft
01.08.2003
Report
Keine Angabe
Englisch
Propulsion Education for General Aviation Aircraft
British Library Conference Proceedings | 2002
|Propulsion Education for General Aviation Aircraft
SAE Technical Papers | 2002
|