Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:solid_rocket_motor
|
| gptkbp:burnTime |
130 seconds
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:Italy |
| gptkbp:diameter |
3.4 m
|
| gptkbp:firstFlight |
2022
|
| gptkbp:length |
13.5 m
|
| gptkbp:manufacturer |
gptkb:ArianeGroup
gptkb:Avio |
| gptkbp:mass |
150,000 kg
|
| gptkbp:propulsion |
solid propellant
|
| gptkbp:purpose |
booster
|
| gptkbp:status |
active
|
| gptkbp:successor |
P80 solid rocket motor
|
| gptkbp:thrust |
4,650 kN
|
| gptkbp:usedIn |
gptkb:Vega-C
gptkb:Ariane_6 |
| gptkbp:bfsParent |
gptkb:Ariane_launch_vehicles
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
P120C solid rocket motor
|