SCIENTIAM QUIA OMNES

SCIENTIAM QUIA OMNES

SCIENTIAM QUIA OMNES

SCIENTIAM QUIA OMNES

SCIENTIAM QUIA OMNES

AEROSPACE ENGINEERING

AEROSPACE ENGINEERING

AEROSPACE ENGINEERING

AEROSPACE ENGINEERING

AEROSPACE ENGINEERING

LAUNCH VEHICLE REGISTER

LAUNCH VEHICLE REGISTER

LAUNCH VEHICLE REGISTER

LAUNCH VEHICLE REGISTER

LAUNCH VEHICLE REGISTER

Manufactured in Iran

Manufactured in Iran

Manufactured in Iran

Manufactured in Iran

Manufactured in Iran

ID	Country	Family	Vehicle	AKA	Stages	Total Length	LEO Payload	MEO Payload	GEO Payload	Stage 0	0 Length	0 Engine	0 Quantity	0 Propellant ID	0 Propellant Ox	0 Propellant Fuel	0 Burn Rate	0 Flow Rate	0 Empty	0 Propellant	0 Gross	0 Upper	0 Net	0 VAC Thrust	0 VAC Specific Impulse	0 VAC T-W Ratio	0 SL Thrust	0 SL Specific Impulse	0 SL T-W Ratio	Stage 1	1 Length	1 Engine	1 Quantity	1 Propellant ID	1 Propellant Ox	1 Propellant Fuel	1 Burn Rate	1 Flow Rate	1 Empty	1 Propellant	1 Gross	1 Upper	1 Net	1 VAC Thrust	1 VAC Specific Impulse	1 VAC T-W Ratio	1 SL Thrust	1 SL Specific Impulse	1 SL T-W Ratio	Stage 2	2 Length	2 Engine	2 Quantity	2 Propellant ID	2 Propellant Ox	2 Propellant Fuel	2 Burn Rate	2 Flow Rate	2 Empty	2 Propellant	2 Gross	2 Upper	2 Net	2 VAC Thrust	2 VAC Specific Impulse	2 VAC T-W Ratio	2 SL Thrust	2 SL Specific Impulse	2 SL T-W Ratio	Stage 3	3 Length	3 Engine	3 Quantity	3 Propellant ID	3 Propellant Ox	3 Propellant Fuel	3 Burn Rate	3 Flow Rate	3 Empty	3 Propellant	3 Gross	3 Upper	3 Net	3 VAC Thrust	3 VAC Specific Impulse	3 VAC T-W Ratio	3 SL Thrust	3 SL Specific Impulse	3 SL T-W Ratio	Stage 4	4 Length	4 Engine	4 Quantity	4 Propellant ID	4 Propellant Ox	4 Propellant Fuel	4 Burn Rate	4 Flow Rate	4 Empty	4 Propellant	4 Gross	4 Upper	4 Net	4 VAC Thrust	4 VAC Specific Impulse	4 VAC T-W Ratio	4 SL Thrust	4 SL Specific Impulse	4 SL T-W Ratio	Stage 5	5 Length	5 Engine	5 Quantity	5 Propellant ID	5 Propellant Ox	5 Propellant Fuel	5 Burn Rate	5 Flow Rate	5 Empty	5 Propellant	5 Gross	5 VAC Thrust	5 VAC Specific Impulse	5 VAC T-W Ratio	5 SL Thrust	5 SL Specific Impulse	5 SL T-W Ratio
1	IRN	SHAHAB	Safir-1	-	3	31.14	25.00	-	-													20,300	20,300							Safir-1 (1)	13.50	Safir-1	1	NTO-UDMH	Liquid	Liquid	160.00	77.50	2,600	12,400	15,000	5,300	20,300	225.00	296.05	16.99	192.61	253.43	14.55	Safir-1 (2)	8.50	Safir-2	1	NTO-UDMH	Liquid	Liquid	390.00	12.05	300	4,700	5,000	300	5,300	40.00	338.46	20.39	34.24	289.74	17.46	Safir-1 (3)	9.14	Safir-3	1	AP-HTPB-Al	Solid	Solid	100.00	2.50	50	250	300		300	8.00	326.31	16.31	6.85	279.34	13.97
2	IRN	SHAHAB	Safir-1A	-	3	31.14	15.00	-	-													20,300	20,300							Safir-1A (1)	13.50	Safir-1	1	NTO-UDMH	Liquid	Liquid	160.00	77.50	2,600	12,400	15,000	5,300	20,300	225.00	296.05	16.99	192.61	253.43	14.55	Safir-1A (2)	8.50	Safir-2	1	NTO-UDMH	Liquid	Liquid	390.00	12.05	300	4,700	5,000	300	5,300	40.00	338.46	20.39	34.24	289.74	17.46	Safir-1A (3)	9.14	Safir-3	1	AP-HTPB-Al	Solid	Solid	100.00	2.50	50	250	300		300	8.00	326.31	16.31	6.85	279.34	13.97
3	IRN	SHAHAB	Safir-1B	-	3	31.14	52.00	-	-													20,300	20,300							Safir-1B (1)	13.50	Safir-1	1	NTO-UDMH	Liquid	Liquid	160.00	77.50	2,600	12,400	15,000	5,300	20,300	225.00	296.05	16.99	192.61	253.43	14.55	Safir-1B (2)	8.50	Safir-2	1	NTO-UDMH	Liquid	Liquid	390.00	12.05	300	4,700	5,000	300	5,300	40.00	338.46	20.39	34.24	289.74	17.46	Safir-1B (3)	9.14	Safir-3	1	AP-HTPB-Al	Solid	Solid	100.00	2.50	50	250	300		300	8.00	326.31	16.31	6.85	279.34	13.97
																																													296.05
ID	Country	Family	Vehicle	AKA	Stages	Total Length	LEO Payload	MEO Payload	GEO Payload	Stage 0	0 Length	0 Engine	0 Quantity	0 Propellant ID	0 Propellant Ox	0 Propellant Fuel	0 Burn Rate	0 Flow Rate	0 Empty	0 Propellant	0 Gross	0 Upper	0 Net	0 VAC Thrust	0 VAC Specific Impulse	0 VAC T-W Ratio	0 SL Thrust	0 SL Specific Impulse	0 SL T-W Ratio	Stage 1	1 Length	1 Engine	1 Quantity	1 Propellant ID	1 Propellant Ox	1 Propellant Fuel	1 Burn Rate	1 Flow Rate	1 Empty	1 Propellant	1 Gross	1 Upper	1 Net	1 VAC Thrust	1 VAC Specific Impulse	1 VAC T-W Ratio	1 SL Thrust	1 SL Specific Impulse	1 SL T-W Ratio	Stage 2	2 Length	2 Engine	2 Quantity	2 Propellant ID	2 Propellant Ox	2 Propellant Fuel	2 Burn Rate	2 Flow Rate	2 Empty	2 Propellant	2 Gross	2 Upper	2 Net	2 VAC Thrust	2 VAC Specific Impulse	2 VAC T-W Ratio	2 SL Thrust	2 SL Specific Impulse	2 SL T-W Ratio	Stage 3	3 Length	3 Engine	3 Quantity	3 Propellant ID	3 Propellant Ox	3 Propellant Fuel	3 Burn Rate	3 Flow Rate	3 Empty	3 Propellant	3 Gross	3 Upper	3 Net	3 VAC Thrust	3 VAC Specific Impulse	3 VAC T-W Ratio	3 SL Thrust	3 SL Specific Impulse	3 SL T-W Ratio	Stage 4	4 Length	4 Engine	4 Quantity	4 Propellant ID	4 Propellant Ox	4 Propellant Fuel	4 Burn Rate	4 Flow Rate	4 Empty	4 Propellant	4 Gross	4 Upper	4 Net	4 VAC Thrust	4 VAC Specific Impulse	4 VAC T-W Ratio	4 SL Thrust	4 SL Specific Impulse	4 SL T-W Ratio	Stage 5	5 Length	5 Engine	5 Quantity	5 Propellant ID	5 Propellant Ox	5 Propellant Fuel	5 Burn Rate	5 Flow Rate	5 Empty	5 Propellant	5 Gross	5 VAC Thrust	5 VAC Specific Impulse	5 VAC T-W Ratio	5 SL Thrust	5 SL Specific Impulse	5 SL T-W Ratio

EDUCATIONAL RESOURCE

EDUCATIONAL RESOURCE

EDUCATIONAL RESOURCE

EDUCATIONAL RESOURCE

EDUCATIONAL RESOURCE

SCIENTIAM QUIA OMNES

SCIENTIAM QUIA OMNES

SCIENTIAM QUIA OMNES

SCIENTIAM QUIA OMNES

SCIENTIAM QUIA OMNES