Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:cycle |
expander cycle
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:firstFlight |
1986
|
| gptkbp:fuelType |
liquid hydrogen
|
| gptkbp:length |
2.7 m
|
| gptkbp:manufacturer |
gptkb:IHI_Corporation
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
440 seconds
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:LE-5A
|
| gptkbp:thrustVacuum |
89 kN
|
| gptkbp:usedFor |
gptkb:upper_stage
|
| gptkbp:usedIn |
gptkb:H-II_rocket
gptkb:H-I_rocket |
| gptkbp:weight |
246 kg
|
| gptkbp:bfsParent |
gptkb:IHI_Aerospace
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
LE-5 rocket engine
|