Research on Simulation and Performance Optimization of Mach 4 Civil Aircraft Propulsion Concept

Table 1

Data survey of the concept scheme of the supersonic civil aircraft [1, 3–5, 18, 19].

		(km)		(kg)	(kg)	(kg)	WF (kg)	(kg)	(PAX^·km/kg)
Mach 3	3.0	12,038	250	323,727	24,864	123,822	175,043	99	19.9
Mach 4	4.0	12,038	251	392,656	24,963	138,678	229,015	99	14.9
HSCT BOE MFTF5093	2.4	9260	300	320,051	29,433	124,141	166,477	98	18.8
HSCT BOE ACE701510	2.4	9260	300	323,914	29,434	123,918	170,562	98	18.5