Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket engine family
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:fuelType |
LOX/LH2 (HM7B engine)
UDMH/N2O4 (Viking engines) |
| https://www.w3.org/2000/01/rdf-schema#label |
Ariane 4 rocket engines
|
| gptkbp:manufacturer |
gptkb:Aérospatiale
|
| gptkbp:notableModel |
gptkb:HM7B
gptkb:Viking_2 gptkb:Viking_4 |
| gptkbp:status |
retired
|
| gptkbp:thrust |
HM7B: ~62.7 kN
Viking 2: ~667 kN Viking 4: ~667 kN |
| gptkbp:usedIn |
Ariane 4 launch vehicle
|
| gptkbp:usedOnBoosters |
solid rocket boosters
liquid rocket boosters |
| gptkbp:usedOnFirstFlight |
1988
|
| gptkbp:usedOnLastFlight |
2003
|
| gptkbp:usedOnStages |
first stage
third stage second stage |
| gptkbp:bfsParent |
gptkb:National_Space_Centre,_Leicester
|
| gptkbp:bfsLayer |
7
|