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gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
3
|
|
gptkbp:bfsParent
|
gptkb:Saturn_V
|
|
gptkbp:aircraft_operated
|
gptkb:Apollo_14
gptkb:Apollo_16
gptkb:Apollo_6
gptkb:Apollo_2
gptkb:Apollo_3
gptkb:Apollo_0
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_7
gptkb:Apollo_11
gptkb:Apollo_13
gptkb:Apollo_5
gptkb:Apollo_12
gptkb:Apollo_4
gptkb:Apollo_1
|
|
gptkbp:average_temperature
|
3,300 ° F
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:debut_year
|
gptkb:1965
|
|
gptkbp:design
|
gptkb:Rocketdyne
|
|
gptkbp:developer
|
$18 million
|
|
gptkbp:emissions_standard
|
bell nozzle
|
|
gptkbp:engine
|
gptkb:5
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:first_flight
|
gptkb:1967
|
|
gptkbp:fuel_capacity
|
12.2 ft
19.5 ft
|
|
gptkbp:fuel_type
|
gptkb:RP-1
gas-generator cycle
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F-1 engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:investment
|
60 atm
|
|
gptkbp:mission
|
gptkb:software
|
|
gptkbp:number_of_rooms
|
single chamber
70 atm
|
|
gptkbp:produced_by
|
15 engines
|
|
gptkbp:propulsion
|
263 seconds
1,500,000 lbf
81:1
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:successor
|
gptkb:F-1_B
|
|
gptkbp:used_in
|
gptkb:Saturn_V
|
|
gptkbp:water_source
|
12,000 lb/min
29,000 lb/min
|
|
gptkbp:weight
|
18,500 lb
|