Satellite Launch Vehicle Platforms

7 Satellite Launch Vehicle Platforms from 3 Manufacturers meet your specification.
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  • Manufacturers: Aphelion Orbitals, PLD Space, SpaceX
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
Description:MIURA 1 is a suborbital launch vehicle, privately developed in Europe. The first space system is fully designed by PLD Space to take your payloads into space and bring them back safely
Launch Vehicle Diameter:
0.7 m
Launch Vehicle Height:
12.5 m
Payload Capacity:
100 Kg
Number of Stage:
Single Stage
First Stage Engine:
TEPREL-B Liquid Bi-propellant Engine
First Stage Engine Thrust:
30000 N
Propellant:
Kerosene, LOX
Altitude of Apogee:
150 Km
more info
Description:MIURA 5 is a reusable orbital microlauncher, privately developed and designed by PLD Space. This vehicle is dedicated to small satellites, ranging from CubeSats to Class 1 payloads
Launch Vehicle Diameter:
2 m
Launch Vehicle Height:
34.4 m
Payload Capacity:
450 Kg
Number of Stage:
Two Stage
First Stage Engine Thrust:
105000 N
Second Stage Engine Thrust:
45000 N
Propellant:
Kerosene, LOX
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