Satellite Launch Vehicle Platforms

33 Satellite Launch Vehicle Platforms for Space Applications from 12 manufacturers listed on SatNow

Satellite Launch Vehicle Platforms for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

33 Satellite Launch Vehicle Platforms from 12 Manufacturers
33 Products from 12 Manufacturers
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Description:Light Weight Launch Vehicle Platform

Product Specs

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:SkyHy is a two-stage, hybrid, suborbital launch vehicle.

Product Specs

Launch Vehicle Diameter:
0.196 m, 0.153 m (second stage)
Payload Capacity:
Up to2 Kg
Number of Stage:
Three-Stage
First Stage Engine Thrust:
7.3 kN
First Stage Engine ISP:
191 Sec
Second Stage Engine Thrust:
1.95 kN
Second Stage Engine ISP:
192 Sec
Propellant:
HTPB
more info
Description:Electron Launch Vehicle Platform

Product Specs

Launch Vehicle Mass:
13000 Kg
Launch Vehicle Diameter:
1.20 m
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
Altitude of Apogee:
15 Km
Altitude of Perigee:
15 Km
Space Heritage:
Yes
more info
Description:Suborbital Launch Vehicle for Payload Validation

Product Specs

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
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Description:Heavy-Lift Orbital Launch Vehicle

Product Specs

Launch Vehicle Mass:
705000 Kg
Launch Vehicle Diameter:
4.1 m
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:Launch Vehicle for Satellite Missions

Product Specs

Launch Vehicle Mass:
289 Metric Tons
Launch Vehicle Diameter:
4 to 5.1 m
Launch Vehicle Height:
53 m
Payload Capacity:
2970 to 5100 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:Launch Vehicle Platform for Multi-Orbit Operations

Product Specs

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
Description:Flight-Proven Launch Vehicle Platform

Product Specs

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
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Description:Satellite Launch Vehicle Platform for LEO

Product Specs

Launch Vehicle Diameter:
3.35 m
Launch Vehicle Height:
22.3 m
Payload Capacity:
500 Kg
Number of Stage:
Single Stage
First Stage Engine:
STAR-3D Engine
Propellant:
Hybrid (HDPE Fuel / LOx)
more info
Description:Orbital Class Reusable Launch Vehicle Platform

Product Specs

Launch Vehicle Mass:
549054 Kg
Launch Vehicle Diameter:
3.70 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:Heavy-Lift Reusable Launch Vehicle

Product Specs

Launch Vehicle Diameter:
7 m
Launch Vehicle Height:
98 m
Payload Capacity:
13 to 45 metric tons
Number of Stage:
Two Stage
First Stage Engine:
BE-4 Engine
First Stage Engine Thrust:
550000 lbf
Second Stage Engine:
BE-3U Engine
Second Stage Engine Thrust:
160000 lbf
Propellant:
LOX, LNG
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:Ariane 5 is capable of carry payloads weighing more than 10 metric tons to GTO

Product Specs

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: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:Neutron is designed for mega constellation deployment, deep space missions, and human spaceflight

Product Specs

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
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