Reaction Motors XLR-11 rocket engine
GPTKB entity
Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
4
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
pressure-fed
|
| gptkbp:diameter |
0.46 m
|
| gptkbp:firstFlight |
1947
|
| gptkbp:fuelType |
ethyl alcohol
|
| https://www.w3.org/2000/01/rdf-schema#label |
Reaction Motors XLR-11 rocket engine
|
| gptkbp:length |
1.6 m
|
| gptkbp:manufacturer |
gptkb:Reaction_Motors,_Inc.
|
| gptkbp:notableFor |
powered first supersonic flight
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:beer
liquid oxygen |
| gptkbp:status |
retired
|
| gptkbp:throttleable |
no
|
| gptkbp:thrust |
6,000 lbf
|
| gptkbp:usedBy |
gptkb:US_Air_Force
gptkb:NACA |
| gptkbp:usedIn |
gptkb:Convair_XF-92
gptkb:Bell_X-1 gptkb:Douglas_D-558-2_Skyrocket gptkb:Northrop_X-4_Bantam gptkb:Republic_XF-91_Thunderceptor gptkb:X-15_(early_flights) |
| gptkbp:weight |
210 kg
|
| gptkbp:bfsParent |
gptkb:X-24A
gptkb:Lockheed_Martin_X-24 |
| gptkbp:bfsLayer |
7
|