Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:burnTime |
667 seconds
|
| gptkbp:countryOfOrigin |
gptkb:Italy
|
| gptkbp:diameter |
1.9 m
|
| gptkbp:firstFlight |
2012
|
| gptkbp:fuelType |
UDMH
|
| gptkbp:fullName |
gptkb:Attitude_Vernier_Upper_Module
|
| https://www.w3.org/2000/01/rdf-schema#label |
AVUM
|
| gptkbp:length |
1.7 m
|
| gptkbp:manufacturer |
gptkb:Avio
|
| gptkbp:mass |
1200 kg
|
| gptkbp:oxidizer |
N2O4
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:purpose |
upper stage propulsion
|
| gptkbp:status |
active
|
| gptkbp:thrustVacuum |
2.45 kN
|
| gptkbp:usedOn |
gptkb:Vega_rocket
|
| gptkbp:bfsParent |
gptkb:Vega_rocket
|
| gptkbp:bfsLayer |
6
|