Satellite Launch Vehicle Platforms

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Trailblazer allows the payload to be externally deployed

Satellite Launch Vehicle Platform from Aphelion Orbitals

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SKU:Trailblazer

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

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Aphelion Orbitals - Helios

Satellite Launch Vehicle Platform from Aphelion Orbitals

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Description:Helios offers full integration with Cassiopeia line of modular Cubesat components and software products

Launch Vehicle Mass:

3510 Kg

Launch Vehicle Diameter:

0.8 m

Launch Vehicle Height:

10.3 m

Payload Capacity:

20 Kg

Number of Stage:

Three Stage

First Stage Engine:

Hypergolic Aerospike Engine

First Stage Engine Thrust:

45000 N

Second Stage Engine Thrust:

9500 N

Propellant:

Hypergolic Propellant

Altitude of Apogee:

400 Km

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International Launch Services - Proton Breeze M

Satellite Launch Vehicle Platform from International Launch Services

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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

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International Launch Services - Angara 1.2

Satellite Launch Vehicle Platform from International Launch Services

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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

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United Launch Alliance - Atlas V 400 Series

Satellite Launch Vehicle Platform from United Launch Alliance

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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

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United Launch Alliance - Atlas V 500 Series

Satellite Launch Vehicle Platform from United Launch Alliance

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Description:Atlas V 500 Series uses a standard common core booster, a Centaur upper stage in a single or dual-engine configuration

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

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

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

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

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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United Launch Alliance - Delta II

Satellite Launch Vehicle Platform from United Launch Alliance

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

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

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PLD Space - MIURA 1

Satellite Launch Vehicle Platform from PLD Space

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Description:MIURA 1 is a suborbital launch vehicle, privately developed in Europe. The first space system is fully designed by PLD Space to take your payloads into space and bring them back safely

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

Satellite Launch Vehicle Platforms

Trailblazer allows the payload to be externally deployed

Aphelion Orbitals - Helios

International Launch Services - Proton Breeze M

International Launch Services - Angara 1.2

United Launch Alliance - Atlas V 400 Series

United Launch Alliance - Atlas V 500 Series

United Launch Alliance - Vulcan

United Launch Alliance - Delta IV

United Launch Alliance - Delta II

PLD Space - MIURA 1

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Satellite Launch Vehicle Platforms

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Manufacturers

Launch Vehicle Mass (m)

Launch Vehicle Diameter (m)

Launch Vehicle Height (m)

Payload Capacity (Kg)

Space Heritage

Quick Links

Popular Categories

Satellite Calculators

Our Network

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Let us know what you need? We can identify products or connect you with appropriate suppliers.

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