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	ISR	Israel Aerospace Industries	LK-1	-	AP-HTPB-Al	Solid	Solid	1	5,900	0.45	1.35	9 : 1	1,240.00	774.00	63.65	605.63	49.80
2	ISR	Israel Aerospace Industries	RSA-3-1	-	AP-HTPB-Al	Solid	Solid	1	5,900	0.23	1.30	31 : 1	1,100.00	456.00	42.27	391.16	36.26
3	ISR	Israel Aerospace Industries	RSA-3-2	-	AP-HTPB-Al	Solid	Solid	1	5,900	0.23	1.30	31 : 1	1,771.00	476.70	27.45	408.91	23.54
4	ISR	Israel Aerospace Industries	RSA-3-3	-	AP-HTPB-Al	Solid	Solid	1	5,900	0.23	1.30	31 : 1	170.00	58.80	35.27	50.44	30.25
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