Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:cycle |
expander bleed cycle
|
| gptkbp:diameter |
2.5 m
|
| gptkbp:engineType |
cryogenic
|
| gptkbp:firstFlight |
2001
|
| https://www.w3.org/2000/01/rdf-schema#label |
LE-5B
|
| gptkbp:length |
3.3 m
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:predecessor |
gptkb:LE-5A
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:specificImpulseVacuum |
448 seconds
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:LE-5B-3
|
| gptkbp:thrustVacuum |
1378 kN
|
| gptkbp:usedFor |
upper stage
|
| gptkbp:usedIn |
gptkb:H-IIA_rocket
gptkb:H-IIB_rocket |
| gptkbp:bfsParent |
gptkb:H-IIB
gptkb:H-IIA_202 |
| gptkbp:bfsLayer |
6
|