Satellite Launch Vehicle Platforms - Yes

16 Satellite Launch Vehicle Platforms from 6 Manufacturers meet your specification.
Selected Filters Reset All
  • Space Heritage: Yes
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:Ariane 5 is capable of carry payloads weighing more than 10 metric tons to GTO
Launch Vehicle Mass:
780 Kg
Launch Vehicle Diameter:
5.4 m
Launch Vehicle Height:
50.5 m
Payload Capacity:
10000 Kg
Number of Stage:
Two Stage
First Stage Engine:
Cryogenic Engine
Inclination:
6 Degrees
Altitude of Apogee:
35.943 Km
Altitude of Perigee:
250 Km
Space Heritage:
Yes
more info
Description:Ariane 6 launcher provides new levels of efficiency and flexibility to meet customers’ launch services
Payload Capacity:
1.7 to 21.6 Kg
Number of Stage:
Two Stage
First Stage Engine:
Vulcan Engine
Second Stage Engine:
Vinci Engine
Booster:
P120C
Inclination:
5 to 97.5 Degrees
Altitude of Apogee:
35.786 Km
Altitude of Perigee:
250 Km
Space Heritage:
Yes
more info
Description:Vega was purpose-designed for the launch of small scientific or Earth observation satellites
Launch Vehicle Mass:
137 Kg
Launch Vehicle Diameter:
3.025 m
Launch Vehicle Height:
29.9 m
Payload Capacity:
1360 Kg
Number of Stage:
Three Stage
First Stage Engine:
P80 Engine
Second Stage Engine:
Zeifro-23 Engine
Altitude of Apogee:
800 Km
Space Heritage:
Yes
more info
Description:Vega C can be adapted for a broad range of missions from nanosatellites to larger optical and radar observation spacecraft
Launch Vehicle Mass:
190509 Kg
Launch Vehicle Diameter:
3.4 m
Launch Vehicle Height:
35 m
Payload Capacity:
1995 to 2993 Kg
Number of Stage:
Three Stage
Space Heritage:
Yes
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:Atlas V 400 Series uses a standard common core booster, a Centaur upper stage in a single or dual-engine configuration
Payload Capacity:
1935 to 13250 Kg
Number of Stage:
Two Stage
First Stage Engine:
RD 180 Engine
First Stage Engine Thrust:
860300 lbs
First Stage Engine ISP:
311 Seconds
Second Stage Engine:
RL10 Engine
Second Stage Engine Thrust:
22900 lbs
Second Stage Engine ISP:
450.5 Seconds
Propellant:
Liquid Oxygen, Liquid Kerosene, Liquid Hydrogen
Booster:
Aerojet Rocketdyne Solid Rocket Booster
Inclination:
0 Degrees (GEO), 27 Degrees (GTO), 28.7 Degrees (LEO), 90 Degrees (LEO), 51.6 Degrees (LEO ISS)
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