Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:solid_rocket_motor
|
| gptkbp:burnTime |
approximately 120 seconds
|
| gptkbp:countryOfOrigin |
gptkb:Italy
|
| gptkbp:diameter |
1.9 m
|
| gptkbp:firstFlight |
2022
|
| gptkbp:length |
7.6 m
|
| gptkbp:manufacturer |
gptkb:Avio
|
| gptkbp:mass |
approximately 26,000 kg
|
| gptkbp:numberOfStages |
second stage
|
| gptkbp:propulsion |
gptkb:stone
|
| gptkbp:thrust |
1100 kN
|
| gptkbp:usedBy |
gptkb:European_Space_Agency
|
| gptkbp:usedIn |
gptkb:Vega_C
|
| gptkbp:bfsParent |
gptkb:Bombardier_Zefiro
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Zefiro 300
|