Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:cycle |
oxidizer-rich staged combustion
|
| gptkbp:diameter |
0.84 m
|
| gptkbp:firstFlight |
2015
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:gimbalRange |
±10°
|
| https://www.w3.org/2000/01/rdf-schema#label |
YF-115
|
| gptkbp:length |
2.1 m
|
| gptkbp:manufacturer |
gptkb:Academy_of_Aerospace_Liquid_Propulsion_Technology
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
284.5 s
341.5 s |
| gptkbp:status |
in service
|
| gptkbp:thrustSeaLevel |
117 kN
|
| gptkbp:thrustVacuum |
176 kN
|
| gptkbp:usedIn |
gptkb:Long_March_6
gptkb:Long_March_7 gptkb:Long_March_8 |
| gptkbp:weight |
790 kg
|
| gptkbp:bfsParent |
gptkb:Long_March_6
gptkb:Long_March_7 |
| gptkbp:bfsLayer |
6
|