Hypersonic Technology Vehicle 2
GPTKB entity
Statements (64)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
hypersonic vehicle
|
| gptkbp:airlines |
over 30 kilometers
|
| gptkbp:analyzes |
post-flight analysis conducted
|
| gptkbp:collaborations |
gptkb:DARPA
partnerships with universities |
| gptkbp:collection |
aerodynamic performance data
|
| gptkbp:controls |
canards
autonomous guidance system |
| gptkbp:dataTransmission |
real-time telemetry
|
| gptkbp:design |
aerodynamics and thermodynamics
streamlined shape for reduced drag |
| gptkbp:developedBy |
NASA
|
| gptkbp:environmentalImpact |
minimal emissions during flight
|
| gptkbp:firstFlight |
3
approximately 10 minutes 2010-04-22 limited to a few flights per year successful data acquisition valuable insights for future designs multiple_sites_in_the_USA |
| gptkbp:fuelType |
liquid oxygen and kerosene
|
| gptkbp:funding |
gptkb:United_States_government
|
| gptkbp:futurePlans |
advancements in space exploration
|
| gptkbp:hasArea |
gptkb:Pacific_Ocean
flight testing successful hypersonic flight |
| gptkbp:historicalResearch |
hypersonic propulsion systems
|
| https://www.w3.org/2000/01/rdf-schema#label |
Hypersonic Technology Vehicle 2
|
| gptkbp:impact |
potential military applications
|
| gptkbp:internationalRelations |
global hypersonic research initiatives
|
| gptkbp:keyIssues |
data on hypersonic aerodynamics
|
| gptkbp:launchDate |
2010-04-22
|
| gptkbp:launchSite |
gptkb:Wallops_Flight_Facility
Minotaur IV rocket |
| gptkbp:legacy |
pioneering hypersonic flight research
|
| gptkbp:length |
4.5 meters
|
| gptkbp:maxSpeed |
gptkb:Mach_20
|
| gptkbp:missions |
approximately 10 minutes
suborbital_trajectory |
| gptkbp:operationalArea |
not operationally deployed
|
| gptkbp:operationalRange |
over 1,000 kilometers
|
| gptkbp:operationalStatus |
limited to experimental use
no longer in active testing |
| gptkbp:performance |
speed, altitude, and range
|
| gptkbp:primaryMission |
validate hypersonic flight technologies
|
| gptkbp:project |
2011
2003 to 2011 enhance national security capabilities |
| gptkbp:provides |
inertial navigation system
|
| gptkbp:publications |
research papers on hypersonic technology
|
| gptkbp:purpose |
testing hypersonic flight technologies
|
| gptkbp:relatedPatent |
X-43A
|
| gptkbp:research |
federal grants
|
| gptkbp:researchField |
aerospace engineering
|
| gptkbp:researchInterest |
civilian and military uses
|
| gptkbp:retirementYear |
2011-06-30
|
| gptkbp:safetyFeatures |
extensive pre-flight testing
|
| gptkbp:significance |
advancement in hypersonic research
|
| gptkbp:status |
retired
|
| gptkbp:successor |
Hypersonic_Technology_Vehicle_3
|
| gptkbp:team |
gptkb:NASA_Langley_Research_Center
|
| gptkbp:technology |
thermal protection systems
heat management at high speeds |
| gptkbp:weight |
1,500 kilograms
|