Satellite Launch Vehicle Platforms

12 Satellite Launch Vehicle Platforms from 5 Manufacturers meet your specification.
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  • Manufacturers: Aphelion Orbitals, International Launch Services, Mitsubishi Heavy Industries, 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: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
Description:H2A202 launch vehicle is a high-performance rocket consist of first stage, second stage, fairing, one or two pairs of solid rocket boosters
Launch Vehicle Mass:
289 Metric Tons
Launch Vehicle Height:
53 m
Number of Stage:
Two Stage
First Stage Engine:
LE-7A Engine
First Stage Engine Thrust:
1098000 N
First Stage Engine ISP:
440 Seconds
Second Stage Engine:
LE-5B Engine
Second Stage Engine Thrust:
137000 N
Second Stage Engine ISP:
448 Seconds
Booster:
Solid Rocket Booster - A
Space Heritage:
Yes
more info
Description:H2A204 launch vehicle is a high-performance rocket consist of first stage, second stage, fairing, one or two pairs of solid rocket boosters
Launch Vehicle Mass:
442 Metric Tons
Launch Vehicle Height:
53 m
Number of Stage:
Two Stage
First Stage Engine:
LE-7A Engine
First Stage Engine Thrust:
1098000 N
First Stage Engine ISP:
440 Seconds
Second Stage Engine:
LE-5B Engine
Second Stage Engine Thrust:
137000 N
Second Stage Engine ISP:
448 Seconds
Booster:
Solid Rocket Booster - A
Space Heritage:
Yes
more info
Description:H3 provides more launch opportunities by shortening the lead-time from contract to launch
Launch Vehicle Height:
63 m
Payload Capacity:
6500 Kg
Number of Stage:
Two Stage
First Stage Engine:
LE-9 Engine
Second Stage Engine:
LE-5B Engine
Second Stage Engine Thrust:
137000 N
Second Stage Engine ISP:
448 Seconds
Booster:
Solid Rocket Booster - A
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

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