|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
3
|
|
gptkbp:bfsParent
|
gptkb:Saturn_V
|
|
gptkbp:application
|
upper stage propulsion
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:designed_by
|
gptkb:Rocketdyne
|
|
gptkbp:developer
|
gptkb:NASA
1955-1966
|
|
gptkbp:engine
|
retired
staged combustion
single chamber
single combustion chamber
230,000 lbf
upper stage propulsion
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:first_flight
|
gptkb:1966
gptkb:1975
|
|
gptkbp:fuel_capacity
|
15.5 ft
3,000 lb
8.4 ft
|
|
gptkbp:fuel_type
|
gas-generator cycle
liquid bipropellant
liquid oxygen and RP-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
J-2 engine
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
gptkb:Saturn_IB
gptkb:Saturn_I
|
|
gptkbp:mission
|
gptkb:Skylab
gptkb:Apollo_10
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_11
gptkb:Apollo_13
|
|
gptkbp:number_of_rooms
|
gptkb:musical
60 psi
|
|
gptkbp:operated_by
|
gptkb:NASA
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:propulsion
|
263 seconds
75:1
230,000 lbf
|
|
gptkbp:rate_of_fire
|
150 seconds
|
|
gptkbp:replaced_by
|
gptkb:J-2_X_engine
|
|
gptkbp:successor
|
gptkb:J-2_X
|
|
gptkbp:type
|
liquid-fueled
|
|
gptkbp:used_in
|
gptkb:Saturn_V
gptkb:Saturn_IB
gptkb:Saturn_I
|
|
gptkbp:weight
|
3,000 lb
|