Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:application |
launch vehicles
|
| gptkbp:check_in_time |
600 s
|
| gptkbp:combustor_type |
staged combustion
|
| gptkbp:cooling_system |
regenerative cooling
|
| gptkbp:designed_by |
gptkb:Arianespace
|
| gptkbp:development |
gptkb:European_Space_Agency
|
| gptkbp:diameter |
1.5 m
|
| gptkbp:first_flight |
gptkb:1996
|
| gptkbp:fuel_type |
liquid hydrogen
|
| https://www.w3.org/2000/01/rdf-schema#label |
HM7 A engine
|
| gptkbp:length |
3.5 m
|
| gptkbp:number_of_rooms |
gptkb:1
6.5 MPa |
| gptkbp:operational_since |
gptkb:1996
|
| gptkbp:oxidation_states |
liquid oxygen
|
| gptkbp:propulsion |
75 k N
|
| gptkbp:specific_impulse |
450 s
|
| gptkbp:status |
in service
|
| gptkbp:successor |
Vinci engine
|
| gptkbp:type |
liquid hydrogen/liquid oxygen engine
|
| gptkbp:used_in |
gptkb:Ariane_5
|
| gptkbp:weight |
200 kg
|
| gptkbp:bfsParent |
gptkb:H-IIA_253
gptkb:H-IIA_291 gptkb:H-IIA_295 gptkb:H-IIA_209 gptkb:H-IIA_242 gptkb:H-IIA_244 |
| gptkbp:bfsLayer |
5
|