Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:cycle |
expander bleed cycle
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:firstFlight |
1994
|
| gptkbp:fuelType |
liquid hydrogen
|
| https://www.w3.org/2000/01/rdf-schema#label |
LE-5A
|
| gptkbp:length |
3.38 m
|
| gptkbp:manufacturer |
gptkb:IHI_Corporation
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
447 s
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:LE-5B
|
| gptkbp:thrustVacuum |
107.8 kN
|
| gptkbp:usedIn |
gptkb:H-II_rocket
|
| gptkbp:bfsParent |
gptkb:LE-5_rocket_engine
gptkb:H-II_rocket_family gptkb:H-II_rocket gptkb:H-II gptkb:LE-5B |
| gptkbp:bfsLayer |
7
|