Satellite Launch Vehicle Platforms

5 Satellite Launch Vehicle Platforms from 2 Manufacturers meet your specification.
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  • Manufacturers: SpaceX, Aphelion Orbitals
SKU:Trailblazer
Launch Vehicle Mass:
452 Kg
Launch Vehicle Diameter:
0.31 m
Launch Vehicle Height:
6.5 m
Payload Capacity:
20 Kg
Number of Stage:
Single Stage
First Stage Engine:
AO-H1 Engine
First Stage Engine Thrust:
9500 N
Second Stage Engine Thrust:
14000 N
Propellant:
Hypergolic Green Propellant
Inclination:
85 Degrees
Altitude of Apogee:
130 Km
more info
Description:Helios offers full integration with Cassiopeia line of modular Cubesat components and software products
Launch Vehicle Mass:
3510 Kg
Launch Vehicle Diameter:
0.8 m
Launch Vehicle Height:
10.3 m
Payload Capacity:
20 Kg
Number of Stage:
Three Stage
First Stage Engine:
Hypergolic Aerospike Engine
First Stage Engine Thrust:
45000 N
Second Stage Engine Thrust:
9500 N
Propellant:
Hypergolic Propellant
Altitude of Apogee:
400 Km
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