SCIENTIAM QUIA OMNES

AEROSPACE ENGINEERING

ID	Country	Manufacturer	Engine	AKA	Propellant ID	Oxidiser	Fuel	Chambers	Chamber Pressure	Nozzle Diameter Initial	Nozzle Diameter Exit	Nozzle Expansion Ratio	Engine Weight	Vacuum Thrust	V Thrust Weight Ratio	Sea Level Thrust	SL Thrust Weight Ratio
1	ENG	Bristol Siddeley	Gamma-2	-	HP95-Kerosene	Liquid	Liquid	2	4,740	0.63	1.98	10 : 1	173.00	68.20	40.20	64.60	38.08
2	ENG	Bristol Siddeley	Gamma-8	-	HP95-Kerosene	Liquid	Liquid	4	4,740	0.63	1.98	10 : 1	342.00	234.80	70.01	222.40	66.31
3	ENG	Bristol Siddeley	Waxwing	-	TP-H-8299	Solid	Solid	1	4,740	0.22	0.71	10 : 1	87.00	29.40	34.46	25.90	30.36
4	ENG	Rolls-Royce	L-1011	Stargazer	JP-5	Gas	Liquid	1	2,665	0.63	2.15	11.5 : 1	4,171.00	187.30	4.58	175.72	4.30
5	ENG	Rolls-Royce	NB-52B	B52 Stratofortress NB-008	JP-5	Gas	Liquid	1	2,665	0.63	2.15	11.5 : 1	4,171.00	53.80	1.32	48.90	1.20
6	ENG	Rolls Royce	RZ-2	-	LOx-Kerosene	Liquid	Liquid	1	3,946	0.54	1.53	8 : 1	750.00	836.30	113.70	735.50	100.00
ID	Country	Manufacturer	Engine	AKA	Propellant ID	Oxidiser	Fuel	Chambers	Chamber Pressure	Nozzle Diameter Initial	Nozzle Diameter Exit	Nozzle Expansion Ratio	Engine Weight	Vacuum Thrust	V Thrust Weight Ratio	Sea Level Thrust	SL Thrust Weight Ratio