|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:aircraft_operated
|
gptkb:Saturn_launch_vehicle_family
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:designated_as
|
gptkb:J-2
|
|
gptkbp:developed_by
|
gptkb:Rocketdyne
|
|
gptkbp:developer
|
1955-1966
|
|
gptkbp:diameter
|
5 ft 4 in
|
|
gptkbp:emissions_standard
|
bell nozzle
|
|
gptkbp:engine
|
vertical
gas-generator cycle
single engine
|
|
gptkbp:engine_type
|
liquid-fueled engine
|
|
gptkbp:first_flight
|
gptkb:1965
gptkb:1966
gptkb:1975
|
|
gptkbp:fuel_type
|
liquid hydrogen
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
J-2
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:length
|
18 ft 6 in
|
|
gptkbp:mission
|
gptkb:Skylab
gptkb:Apollo-Soyuz_Test_Project
gptkb:software
|
|
gptkbp:number_built
|
more than 30
|
|
gptkbp:number_of_rooms
|
gptkb:single
|
|
gptkbp:operated_by
|
gptkb:NASA
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:propulsion
|
75:1
230,000 lbf
263 seconds in vacuum
|
|
gptkbp:replaced_by
|
gptkb:J-2_X_engine
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:successor
|
gptkb:J-2_X
|
|
gptkbp:used_in
|
gptkb:Apollo_14
gptkb:Saturn_V
gptkb:Apollo_Lunar_Module
gptkb:Apollo_10
gptkb:Apollo_16
gptkb:Apollo_Service_Module
gptkb:Saturn_IB
gptkb:Skylab_3
gptkb:Skylab_4
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_11
gptkb:Apollo_13
gptkb:Skylab_2
gptkb:Apollo_12
gptkb:Apollo-Soyuz_Test_Project
gptkb:software
gptkb:Saturn_I
Skylab space station
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Saturn_V
gptkb:Saturn_V_rocket
|
|
gptkbp:bfsLayer
|
3
|