Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:application |
launch vehicles
|
| gptkbp:combustor_type |
liquid bipropellant
|
| gptkbp:cycle_type |
staged combustion
|
| gptkbp:designed_by |
gptkb:Kuznetsov
|
| gptkbp:development |
ongoing
|
| gptkbp:diameter |
1.5 m
|
| gptkbp:engine_type |
gptkb:Team_Rocket
|
| gptkbp:first_flight |
gptkb:2014
|
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Russian RD-191 engine
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov
|
| gptkbp:number_of_rooms |
one
180 bar |
| gptkbp:operational_status |
in service
|
| gptkbp:oxidation_states |
liquid oxygen
|
| gptkbp:propulsion |
> 200
191 k N |
| gptkbp:specific_impulse |
311 seconds
|
| gptkbp:used_in |
gptkb:Angara_rocket
|
| gptkbp:weight |
approximately 800 kg
|