Multifidelity Multidisciplinary Design Optimization of Integral Solid Propellant Ramjet Supersonic Cruise Vehicles

Table 8

All input parameters.

Disciplines		Parameters	Value
Geometry		Cone length	1500 mm
		Column length	4500 mm
		Diameter	350 mm
		Axial position of inlet	1200 mm
		Length of inlet	2300 mm
		Width of inlet	200 mm
		Height of inlet	150 mm
		Axial position of rudder	5150 mm
		Chord length of rudder root	500 mm
		Chord length of rudder tip	300 mm
		Wingspan of rudder	350 mm
		Thickness of rudder root	100 mm
		Thickness of rudder tip	30 mm
		Diameter of tail	325 mm
Propulsion	Booster	Flow rate	50 kg/s
		Booster length	2000 mm
		Booster specific impulse	204 s
		Burning time	5 s
		Mass of booster	200 kg
			4 MPa
			4
	Gas generator	Gas generator length	2100 mm
		Gas generator total impulse	2600 kNs
		Mass of gas generator	213 kg
		Diameter of nozzle	300 mm
Trajectory		Launch Mach number	2 Mach
		Launch height	10 km
		Cruise height	12 km
		Cruise Mach number	3 Mach
		of climb phase	5°
		of dive phase	5°
		of climb phase	0°
		of dive phase	0°
		Total time	720 s