Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:application |
Conventional runway takeoff and landing
|
| gptkbp:capacity |
75 kg
|
| gptkbp:countryOfOrigin |
gptkb:India
|
| gptkbp:developedBy |
gptkb:Defence_Research_and_Development_Organisation
|
| gptkbp:endurance |
12 hours
|
| gptkbp:engineType |
gptkb:Rotax_914
|
| gptkbp:firstFlight |
2010
|
| gptkbp:length |
8.9 m
|
| gptkbp:manufacturer |
gptkb:Aeronautical_Development_Establishment
|
| gptkbp:maximumSpeed |
150 km/h
|
| gptkbp:maxTakeoffWeight |
720 kg
|
| gptkbp:namedAfter |
gptkb:Rustom_Damania
|
| gptkbp:operationalCeiling |
22,000 ft
|
| gptkbp:role |
gptkb:Surveillance
Reconnaissance |
| gptkbp:status |
gptkb:Prototype
|
| gptkbp:successor |
gptkb:Rustom-2
|
| gptkbp:type |
Medium-altitude long-endurance UAV
|
| gptkbp:wingspan |
7.9 m
|
| gptkbp:bfsParent |
gptkb:Rustom_UAV
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rustom-1
|