Satellite Launch Vehicle Engines from Manufacturers in France

9 Satellite Launch Vehicle Engines from 2 Manufacturers meet your specification.
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9 Satellite Launch Vehicle Engines from 2 Manufacturers
9 Products from 2 Manufacturers
Description:It is a European demonstrator for a very low cost, potentially reusable engine

Product Specs

Propellant:
LOX, Methane
more info
Description:Upper Stage Launch Vehicle Engine

Product Specs

Vacuum Thrust:
29.6 kN
Specific Impulse:
324 sec
Engine Mass:
111 Kg (Thrust chamber mass)
Height:
2.2 m
Nozzle Outlet Diameter:
1.31 m
Propellant:
N2O4, MMH
Propellant Flow Rate:
9.3 Kg/sec
Space Heritage:
Yes
more info
Description:Satellite Launch Vehicle Cryogenic Engine

Product Specs

Vacuum Thrust:
64.8 kN
Specific Impulse:
446 sec
Engine Mass:
165 Kg
Height:
2.01 m
Propellant:
LOX-LH2
Propellant Flow Rate:
14.8 Kg/sec
Space Heritage:
Yes
more info
Description:Cryogenic Upper Stage Engine for Space Launchers

Product Specs

Vacuum Thrust:
130 to 180 kN
Specific Impulse:
457.2 to 458.2 sec
Height:
3.22 m
Nozzle Outlet Diameter:
1.84 m
Propellant:
LOX-LH2
Propellant Flow Rate:
24.20 to 34.11 Kg/sec
more info
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Description:Satellite Launch Vehicle Engine for LEO Missions

Product Specs

Vacuum Thrust:
29.6 kN
Specific Impulse:
324 sec
Engine Mass:
111 Kg (Chamber)
Nozzle Outlet Diameter:
1.31 m
Propellant:
N2O4, MMH
Propellant Flow Rate:
9.3 Kg/s
more info
Description:Cryogenic Main Stage Engine

Product Specs

Vacuum Thrust:
1371 kN
Specific Impulse:
432 sec
Height:
3.6 m
Nozzle Outlet Diameter:
2.1 m
Propellant:
LOX-LH2
Propellant Flow Rate:
326 Kg/sec
more info
Description:HM7B engine has recorded a run of 148 consecutive successes

Product Specs

Vacuum Thrust:
64.8 kN
Specific Impulse:
446 sec
Engine Mass:
165 Kg
Height:
2.01 m
Propellant:
Liquid Oxygen, LOX-LH2
Propellant Flow Rate:
14.8 Kg/s
more info
Description:Vinci represents the latest generation of cryogenic upper stage engines for space launchers.

Product Specs

Vacuum Thrust:
130 to 180 kN
Specific Impulse:
457.2 to 458.2 sec
Height:
3.22 m
Nozzle Outlet Diameter:
1.84 m
Propellant:
Liquid Oxygen, LOX-LH2
Propellant Flow Rate:
24.20 / 4.40 to 34.11 /5.59 Kg/s
more info
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Description:The Vulcain 2.1 cryogenic engine provides a thrust of 135 metric tons in a vacuum

Product Specs

Vacuum Thrust:
1, 371 kN
Specific Impulse:
432 sec
Height:
3.6 m
Nozzle Outlet Diameter:
2.1 m
Propellant:
Liquid Oxygen, LOX-LH2
Propellant Flow Rate:
326 Kg/s
more info
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Space Heritage