Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:burnTime |
155 s
|
| gptkbp:chamberPressure |
18 MPa
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:diameter |
1.35 m
|
| gptkbp:engineCycle |
oxidizer-rich staged combustion
|
| gptkbp:firstFlight |
2012
|
| gptkbp:gimbalRange |
±6°
|
| https://www.w3.org/2000/01/rdf-schema#label |
YF-100
|
| gptkbp:length |
2.99 m
|
| gptkbp:manufacturer |
gptkb:Academy_of_Aerospace_Liquid_Propulsion_Technology
|
| gptkbp:nozzleExpansionRatio |
36
|
| gptkbp:propulsion |
kerosene
liquid oxygen |
| gptkbp:status |
in service
|
| gptkbp:thrustSeaLevel |
1,200 kN
|
| gptkbp:thrustVacuum |
1,340 kN
|
| gptkbp:usedIn |
gptkb:satellite
gptkb:Long_March_6 gptkb:Long_March_7 |
| gptkbp:weight |
2,400 kg
|
| gptkbp:bfsParent |
gptkb:CZ-5_(Long_March_5)
gptkb:CZ-6_(Long_March_6) gptkb:Long_March_5B gptkb:Long_March_6 gptkb:Long_March_7 gptkb:Long_March_8 |
| gptkbp:bfsLayer |
6
|