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	KOR	KARI		KSR-1	-	AP-HTPB-Al	Solid	Solid	1	4,426	0.06	0.42	49 : 1	100.00	86.20	87.90	75.86	77.35
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