Launch Vehicle Engines - Arianespace

5 Launch Vehicle Engines from Arianespace meet your specification.
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  • Manufacturers: Arianespace
Description:It is a European demonstrator for a very low cost, potentially reusable engine
Propellant:
LOX, Methane
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Description:The Aestus engine powers the Ariane 5 ES version bipropellant upper stage for insertion of payloads into LEO, SSO and GTO
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
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Description:The HM7B cryogenic engine powers the cryogenic upper stage of Ariane 5 ECA, on which it has performed more than 130 consecutive successful flights
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:Vinci represents the latest generation of cryogenic upper stage engines for space launchers. It is designed to be simple to build and operate
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
Description:This cryogenic engine is being developed by ArianeGroup in cooperation with its European partners on behalf of the ESA It powers the cryogenic main stage of the Ariane 6 launcher for the first eight m...
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

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Space Heritage