|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:check_in_time
|
approximately 60 seconds
|
|
gptkbp:combustor_type
|
gas-generator cycle
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:development
|
1955-1959
|
|
gptkbp:engine_configuration
|
four engines in parallel
|
|
gptkbp:first_flight
|
gptkb:1959
June 8, 1959
|
|
gptkbp:flight_style
|
199
|
|
gptkbp:fuel_type
|
liquid oxygen and kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
XLR11 rocket engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:inspired
|
future rocket engine designs
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:mission
|
gptkb:suborbital_flights
|
|
gptkbp:notable_feature
|
gimbaled thrust
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:number_of_rooms
|
1,000 psi
|
|
gptkbp:operated_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:propulsion
|
57,000 lbf
|
|
gptkbp:specific_impulse
|
265 seconds
|
|
gptkbp:successor
|
gptkb:XLR99_rocket_engine
|
|
gptkbp:type
|
gptkb:Team_Rocket
|
|
gptkbp:used_by
|
gptkb:NASA
|
|
gptkbp:used_in
|
gptkb:X-15_rocket_plane
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Bell_X-1
|
|
gptkbp:bfsLayer
|
4
|