Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
experimental aircraft
|
| gptkbp:annualRidership |
4
|
| gptkbp:collaborations |
NASA
|
| gptkbp:collection |
engine performance
structural integrity aerodynamic performance thermal characteristics |
| gptkbp:construction_cost |
$300 million
|
| gptkbp:controls |
fly-by-wire
|
| gptkbp:elevation |
70,000 feet
|
| gptkbp:engineType |
scramjet
|
| gptkbp:firstFlight |
2003
|
| gptkbp:fuelType |
JP-7
|
| gptkbp:hasArea |
gptkb:Point_Mugu_Naval_Air_Station
|
| https://www.w3.org/2000/01/rdf-schema#label |
X-51
|
| gptkbp:inspiration |
previous scramjet designs
|
| gptkbp:launchSite |
air launch
|
| gptkbp:launchVehicle |
gptkb:B-52_Stratofortress
|
| gptkbp:length |
7.5 meters
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:maximum_speed |
gptkb:Mach_6.8
|
| gptkbp:notable_event |
first air-breathing scramjet to fly for over 3 minutes.
|
| gptkbp:number_of_stages |
Phase 1
Phase 2 Phase 3 |
| gptkbp:operational_status |
retired
military research |
| gptkbp:operationalRange |
over 600 miles
|
| gptkbp:purpose |
hypersonic flight research
|
| gptkbp:research_focus |
hypersonic speeds
|
| gptkbp:successor |
gptkb:Hypersonic_Technology_Vehicle_2
|
| gptkbp:team |
gptkb:Boeing_Phantom_Works
|
| gptkbp:technology |
materials science
advanced materials computational fluid dynamics sensor technology advanced propulsion systems control algorithms aerodynamic modeling autonomous flight systems guidance systems thermal protection systems high-speed data links data telemetry systems hypersonic glide vehicles high-speed wind tunnels robotics in aerospace navigation_systems |
| gptkbp:training |
gptkb:DARPA
|
| gptkbp:weight |
2,500 pounds
|
| gptkbp:wingspan |
3.6 meters
|