Satellite Launch Vehicle Platforms

4 Satellite Launch Vehicle Platforms from 2 Manufacturers meet your specification.
Selected Filters Reset All
  • Manufacturers: Rocket Lab, International Launch Services
Description:Electron is designed to deliver small satellites to precise and unique orbits
Launch Vehicle Mass:
13000 Kg
Launch Vehicle Diameter:
1.2 m/3.9 ft
Launch Vehicle Height:
18 m/59 ft
Payload Capacity:
200 Kg
Number of Stage:
Three Stage
First Stage Engine:
9 Sea-level Rutherford Engine
First Stage Engine Thrust:
190000 N
First Stage Engine ISP:
311 Seconds
Second Stage Engine:
Single Vacuum Rutherford Engine
Second Stage Engine Thrust:
25800 N
Second Stage Engine ISP:
343 Seconds
Propellant:
LOX, Kerosene
Space Heritage:
Yes
more info
Description:Neutron is designed for mega constellation deployment, deep space missions, and human spaceflight
Launch Vehicle Mass:
467000 Kg
Launch Vehicle Diameter:
7 m
Launch Vehicle Height:
40 m/131 ft
Payload Capacity:
13000 Kg
Number of Stage:
Two Stage
First Stage Engine:
7 Archimedes Engine
First Stage Engine Thrust:
5960000 N
Second Stage Engine:
Single Vacuum Archimedes Engine
Second Stage Engine Thrust:
1110000 N
Propellant:
LOX, Methane
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

FiltersReset All

Launch Vehicle Mass (m)

Apply

Launch Vehicle Diameter (m)

Apply

Launch Vehicle Height (m)

Apply

Payload Capacity (Kg)

Apply

Space Heritage