Satellite Launch Vehicle Platforms

5 Satellite Launch Vehicle Platforms from 2 Manufacturers meet your specification.
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  • Manufacturers: SpaceX, International Launch Services
Description:The enhanced performance provided by the commercial Proton Launch Vehicle enables our customers to design and launch heavier and more capable spacecraft while maintaining cost effective mission life t...
Launch Vehicle Mass:
705000 Kg
Launch Vehicle Diameter:
4.1
Launch Vehicle Height:
56.2 to 58.2 m
Payload Capacity:
6270 to 6470 Kg
Number of Stage:
Three Stage
First Stage Engine:
RD-276 Liquid Rocket Engines
First Stage Engine Thrust:
10 MN
Second Stage Engine:
RD-0210 Liquid Rocket Engine, RD-0211 Liquid Rocket Engine, RD-0213 Liquid Rocket Engine
Second Stage Engine Thrust:
2.4 MN
Propellant:
Nitrogen Tetroxide (N2O4) Unsymmetrical DiMethyl Hydrazine (UDMH)
Space Heritage:
Yes
more info
Description:The Angara 1.2 launch vehicle can launch a variety of satellites, weighing up to 3 metric tons, to Low Earth Orbit (LEO)
Payload Capacity:
3000 Kg
Number of Stage:
Two Stage
First Stage Engine:
RD-0191
Second Stage Engine:
RD-0124A Engine
Propellant:
MON, MMH, LOX, Kerosene
Space Heritage:
Yes
more info
SKU:FALCON 9
Launch Vehicle Mass:
549054 Kg
Launch Vehicle Diameter:
3.7 m
Launch Vehicle Height:
70 m
Payload Capacity:
4020 to 22800 Kg
Number of Stage:
Two Stage
First Stage Engine:
Merlin Engine
First Stage Engine Thrust:
845000 N
Second Stage Engine:
Merlin Vaccum Engine
Second Stage Engine Thrust:
981000 N
Propellant:
Kerosene (RP-1), LOX
Space Heritage:
Yes
more info
Description:Falcon Heavy is the most powerful operational rocket in the world by a factor of two. Falcon Heavy can lift more than twice the payload of the next closest operational vehicle, the Delta IV Heavy
Launch Vehicle Mass:
1420788 Kg
Launch Vehicle Diameter:
12.2 m
Launch Vehicle Height:
70 m
Payload Capacity:
16800 to 63800 Kg
Number of Stage:
Two Stage
First Stage Engine:
Merlin Engine
First Stage Engine Thrust:
845000 N
Second Stage Engine:
Merlin Vaccum Engine
Second Stage Engine Thrust:
981000 N
Propellant:
Kerosene (RP-1), LOX
Space Heritage:
Yes
more info
Description:SpaceX’s Starship system represents a fully reusable transportation system designed to service Earth orbit needs as well as missions to the Moon and Mars
Launch Vehicle Diameter:
9 m
Launch Vehicle Height:
50 m
Payload Capacity:
100000 to 150000 Kg
First Stage Engine:
Raptor Engine
First Stage Engine Thrust:
500 klbf
Propellant:
Liquid Methane (CH4), Liquid Oxygen (LOX)
more info

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Space Heritage