Statements (27)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:countryOfOrigin |
gptkb:United_States
|
gptkbp:cycle |
gas-generator
|
gptkbp:diameter |
34 in
|
gptkbp:engineType |
liquid-fueled
|
gptkbp:firstFlight |
1959
|
https://www.w3.org/2000/01/rdf-schema#label |
Reaction Motors XLR99
|
gptkbp:length |
94 in
|
gptkbp:manufacturer |
gptkb:Reaction_Motors
|
gptkbp:notableFeature |
first large, throttleable, restartable, man-rated liquid-propellant rocket engine built in the US
|
gptkbp:propulsion |
liquid oxygen
anhydrous ammonia |
gptkbp:restartable |
yes
|
gptkbp:specificImpulseVacuum |
279 s
|
gptkbp:status |
retired
|
gptkbp:throttleable |
yes
|
gptkbp:thrust |
57,000 lbf
254 kN |
gptkbp:usedBy |
gptkb:NASA
gptkb:US_Air_Force |
gptkbp:usedFor |
gptkb:aircraft
|
gptkbp:usedIn |
gptkb:North_American_X-15
|
gptkbp:weight |
910 lb
|
gptkbp:bfsParent |
gptkb:North_American_X-15
gptkb:X-15_Rocket_Plane gptkb:X-15_rocket_plane |
gptkbp:bfsLayer |
6
|