Hypersonic Technology Vehicle 2 (HTV-2)
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
gptkb:helicopter |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crashLocation |
both test flights ended in loss of vehicle
|
| gptkbp:designedFor |
hypersonic glide
|
| gptkbp:firstFlight |
April 22, 2010
|
| gptkbp:flightNumber |
2
|
| gptkbp:flightTestLocation |
gptkb:Vandenberg_Air_Force_Base
|
| gptkbp:flightTestYear |
2010
2011 |
| https://www.w3.org/2000/01/rdf-schema#label |
Hypersonic Technology Vehicle 2 (HTV-2)
|
| gptkbp:length |
3.7 meters
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:maximumSpeed |
Mach 20
|
| gptkbp:operator |
gptkb:DARPA
|
| gptkbp:partOf |
gptkb:DARPA_Falcon_Project
|
| gptkbp:platform |
Minotaur IV rocket
|
| gptkbp:purpose |
test hypersonic flight
|
| gptkbp:relatedTo |
gptkb:Falcon_Project
gptkb:Prompt_Global_Strike |
| gptkbp:status |
retired
|
| gptkbp:bfsParent |
gptkb:Prompt_Global_Strike_(PGS)_program
gptkb:Common_Aero_Vehicle_(CAV) |
| gptkbp:bfsLayer |
8
|