Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
spaceplane technology demonstrator
|
| gptkbp:application |
unpowered glide landing
|
| gptkbp:countryOfOrigin |
gptkb:India
|
| gptkbp:developedBy |
gptkb:Indian_Space_Research_Organisation
|
| gptkbp:expansion |
orbital re-entry and landing tests
|
| gptkbp:firstFlight |
2016-05-23
|
| gptkbp:fullName |
gptkb:Reusable_Launch_Vehicle-Technology_Demonstrator
|
| https://www.w3.org/2000/01/rdf-schema#label |
RLV-TD
|
| gptkbp:launchSite |
gptkb:Satish_Dhawan_Space_Centre
|
| gptkbp:length |
6.5 meters
|
| gptkbp:missionType |
gptkb:technology
|
| gptkbp:orbitType |
suborbital
|
| gptkbp:propulsion |
piston engine
|
| gptkbp:purpose |
demonstrate technologies for a future reusable launch vehicle
|
| gptkbp:relatedTo |
gptkb:ISRO_Reusable_Launch_Vehicle_program
|
| gptkbp:shape |
delta wing
|
| gptkbp:status |
in development
|
| gptkbp:testFlights |
gptkb:HEX-01
success |
| gptkbp:type |
hypersonic flight experiment
|
| gptkbp:weight |
1.75 tonnes
|
| gptkbp:bfsParent |
gptkb:Reusable_Launch_Vehicle_(RLV)_program
gptkb:Reusable_Launch_Vehicle_program |
| gptkbp:bfsLayer |
6
|