Satellite Launch Vehicle Platforms from Manufacturers in United States

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Rocket Lab - Electron

Satellite Launch Vehicle Platform from Rocket Lab

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

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International Launch Services - Proton Breeze M

Satellite Launch Vehicle Platform from International Launch Services

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

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United Launch Alliance - Atlas V 400 Series

Satellite Launch Vehicle Platform from United Launch Alliance

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

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VayaSpace - Dauntless

Satellite Launch Vehicle Platform from VayaSpace

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)

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SpaceX - FALCON 9

Satellite Launch Vehicle Platform from SpaceX

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

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Blue Origin - New Glenn

Satellite Launch Vehicle Platform from Blue Origin

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

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Rocket Lab - Neutron

Satellite Launch Vehicle Platform from Rocket Lab

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

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International Launch Services - Angara 1.2

Satellite Launch Vehicle Platform from International Launch Services

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

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United Launch Alliance - Atlas V 500 Series

Satellite Launch Vehicle Platform from United Launch Alliance

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

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United Launch Alliance - Vulcan

Satellite Launch Vehicle Platform from United Launch Alliance

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

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United Launch Alliance - Delta IV

Satellite Launch Vehicle Platform from United Launch Alliance

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

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SpaceX - FALCON HEAVY

Satellite Launch Vehicle Platform from SpaceX

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

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SpaceX - Starship

Satellite Launch Vehicle Platform from SpaceX

Description:SpaceX’s Starship system represents a fully reusable transportation system designed to service Earth orbit needs as well as missions to the Moon and Mars

Product Specs

Launch Vehicle Diameter:

9 m

Launch Vehicle Height:

50 m

Payload Capacity:

100000 to 150000 Kg

First Stage Engine:

Raptor Engine

Propellant:

Liquid Methane (CH4), Liquid Oxygen (LOX)

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United Launch Alliance - Delta II

Satellite Launch Vehicle Platform from United Launch Alliance

Description:Delta II has launched many memorable missions including NASA’s rovers Spirit and Opportunity, the Phoenix Mars Lander, all operational GPS missions

Product Specs

Launch Vehicle Height:

39 m/128 ft

Payload Capacity:

1870 to 3470 Kg

Number of Stage:

Three Stage

First Stage Engine:

RS-27 A Engine

Second Stage Engine:

Aerojet AJ10-118K Engine

Second Stage Engine Thrust:

9753 lbs

Second Stage Engine ISP:

320.5 Seconds

Propellant:

Aerozine 50/N204

Space Heritage:

Yes

Related News

Related Products

Satellite Launch Vehicle Platforms from Manufacturers in United States

Rocket Lab - Electron

International Launch Services - Proton Breeze M

United Launch Alliance - Atlas V 400 Series

VayaSpace - Dauntless

SpaceX - FALCON 9

Blue Origin - New Glenn

Rocket Lab - Neutron

International Launch Services - Angara 1.2

United Launch Alliance - Atlas V 500 Series

United Launch Alliance - Vulcan

United Launch Alliance - Delta IV

SpaceX - FALCON HEAVY

SpaceX - Starship

United Launch Alliance - Delta II

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