Statements (14)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:apogee |
100 km
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.16 meters
|
| gptkbp:firstFlight |
1951
|
| gptkbp:launchMass |
62 kg
|
| gptkbp:length |
3.2 meters
|
| gptkbp:manufacturer |
gptkb:Société_d'Etudes_pour_la_Propulsion_par_Réaction_(SEPR)
|
| gptkbp:propulsion |
solid fuel
|
| gptkbp:status |
retired
|
| gptkbp:usedBy |
gptkb:French_military
|
| gptkbp:bfsParent |
gptkb:T-6
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
T-6 (rocket)
|