Satellite Launch Vehicle Platforms - Page 2

33 Satellite Launch Vehicle Platforms from 12 Manufacturers meet your specification.
33 Satellite Launch Vehicle Platforms from 12 Manufacturers
33 Products from 12 Manufacturers
Page 2 of 3
Description:The Angara 1.2 launch vehicle can launch a variety of satellites, weighing up to 3 metric tons, to Low Earth Orbit (LEO)

Product Specs

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:H2A204 launch vehicle is a high-performance rocket consist of first stage, second stage, fairing, one or two pairs of solid rocket boosters

Product Specs

Launch Vehicle Mass:
442 Metric Tons
Launch Vehicle Diameter:
4 to 5.1 m
Launch Vehicle Height:
53 m
Payload Capacity:
4820 to 5950 Kg
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
Propellant:
LH2, LOX
Booster:
Solid Rocket Booster - A
Space Heritage:
Yes
more info
Description:Atlas V 500 Series uses a standard common core booster, a Centaur upper stage in a single or dual-engine configuration

Product Specs

Payload Capacity:
2540 to 18850 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
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

Product Specs

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
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Description:Three Stage Light Class Orbital Launch Vehicle

Product Specs

Launch Vehicle Diameter:
2.2 to 2.20000004768372 m
Payload Capacity:
Up to315 Kg
Number of Stage:
Three-Stage
First Stage Engine Thrust:
70 to 79.6999969482422
First Stage Engine ISP:
250.2 to 284.91 sec
Second Stage Engine Thrust:
85 kN
Second Stage Engine ISP:
306 sec
Propellant:
HTP / KEROSENE
Altitude of Apogee:
200 to 1000 Km
more info
Description:Ariane 6 launcher provides new levels of efficiency and flexibility to meet customers’ launch services

Product Specs

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:Vulcan is available in four standard offering configurations including zero, two, four and six solid rocket booster (SRB) variants

Product Specs

Launch Vehicle Diameter:
5.4 m
Payload Capacity:
2600 to 27200 Kg
Number of Stage:
Two Stage
First Stage Engine:
Blue Origin BE-4 Engine
First Stage Engine Thrust:
550000 lbs
Second Stage Engine:
RL10C Engine
Second Stage Engine Thrust:
24000 lbs
Propellant:
Liquefied Natural Gas (LNG), Liquid Oxygen, Liquid Hydrogen
Booster:
Northrop Grumman Graphite Epoxy Motor (GEM) 63XL Solid Rocket Booster
Inclination:
0 Degrees (GEO), 27 Degrees (GTO), 28.7 Degrees (LEO), 90 Degrees (LEO-Polar), 51.6 Degrees (LEO ISS), 55 Degrees (MEO)
Space Heritage:
Yes
more info

Product Specs

Payload Capacity:
400 to 595 Kg
Altitude of Apogee:
500 Km
Altitude of Perigee:
500 km
more info
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Description:Single-Stage Suborbital Launch Vehicle

Product Specs

Launch Vehicle Diameter:
0.7 m
Payload Capacity:
50 Kg
Number of Stage:
Three-Stage
First Stage Engine Thrust:
31kN (sea level), 35kN ( vacuum)
First Stage Engine ISP:
229 to 272 sec
Propellant:
HTP / KEROSENE
Altitude of Apogee:
102 Km
more info
Description:H3 provides more launch opportunities by shortening the lead-time from contract to launch

Product Specs

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:Delta IV is comprised of a common booster core, a cryogenic upper stage and a 5-meter diameter payload fairing

Product Specs

Launch Vehicle Diameter:
5 m
Payload Capacity:
1840 to 28370 Kg
Number of Stage:
Two Stage
First Stage Engine:
Aerojet Rocketdyne RS-68A Engine
First Stage Engine Thrust:
14876 lbs
First Stage Engine ISP:
362 Seconds
Second Stage Engine:
RL10 Engine
Second Stage Engine Thrust:
24750 lbs
Second Stage Engine ISP:
465.5 Seconds
Propellant:
Liquid Hydrogen, Liquid Oxygen
Booster:
Orbital ATK 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
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

Product Specs

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
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Product Specs

Payload Capacity:
560 to 815 Kg
Altitude of Apogee:
500 Km
Altitude of Perigee:
500 km
more info
Description:Two Stage Supersonic Suborbital Launch Vehicle

Product Specs

Launch Vehicle Diameter:
0.102 m, 0.075 m (Second stage)
Payload Capacity:
Up to1 Kg
Number of Stage:
Three-Stage
First Stage Engine Thrust:
1.56 kN
First Stage Engine ISP:
172 Sec
Second Stage Engine Thrust:
0.84 kN
Second Stage Engine ISP:
181 Sec
Propellant:
HTPB
more info
Description:Launch Vehicle Platform for Multi-orbit Applications

Product Specs

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
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