Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:experimental_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
development of air-to-air missile technology
|
| gptkbp:diameter |
0.56 m
|
| gptkbp:engineType |
gptkb:liquid-fueled_rocket
|
| gptkbp:firstFlight |
1949
|
| gptkbp:guidanceSystem |
radio command guidance
|
| gptkbp:launchWeight |
940 kg
|
| gptkbp:length |
6.04 m
|
| gptkbp:manufacturer |
gptkb:Bell_Aircraft
|
| gptkbp:maximumSpeed |
Mach 2.0
|
| gptkbp:propulsion |
liquid oxygen and kerosene
|
| gptkbp:purpose |
testbed for missile technology
|
| gptkbp:range |
80 km
|
| gptkbp:retired |
1953
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:AIM-4_Falcon
|
| gptkbp:testFlights |
over 30
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:wingspan |
1.81 m
|
| gptkbp:bfsParent |
gptkb:USAF_X-plane_program
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell X-9 Shrike
|