Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:application |
hydro-pneumatic launcher
|
| gptkbp:countryOfOrigin |
gptkb:India
|
| gptkbp:developedBy |
gptkb:Defence_Research_and_Development_Organisation
|
| gptkbp:firstFlight |
2012
|
| gptkbp:guidanceSystem |
autonomous flight with pre-programmed path
|
| gptkbp:length |
2.32 m
|
| gptkbp:maximumSpeed |
0.7 Mach
|
| gptkbp:payload |
miss distance indicator
radar augmentation devices |
| gptkbp:propulsion |
gptkb:gas_turbine_engine
|
| gptkbp:role |
high-speed expendable aerial target
|
| gptkbp:status |
in service
|
| gptkbp:usedBy |
gptkb:Indian_Armed_Forces
|
| gptkbp:wingspan |
2.5 m
|
| gptkbp:bfsParent |
gptkb:Aeronautical_Development_Establishment_(ADE)
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Abhyas
|