F-1 engine

URI: https://gptkb.org/entity/F-1_engine

GPTKB entity

Predicate	Object
gptkbp:instance_of	gptkb:Team_Rocket
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:combustor_type	gas-generator cycle
gptkbp:debut	gptkb:1965
gptkbp:design	gptkb:Rocketdyne
gptkbp:development_cost	$18 million
gptkbp:engine_type	liquid-fueled
gptkbp:exhaust_system	bell nozzle
gptkbp:first_flight	gptkb:1967
gptkbp:fuel_capacity	12.2 ft 19.5 ft
gptkbp:fuel_type	gptkb:RP-1
https://www.w3.org/2000/01/rdf-schema#label	F-1 engine
gptkbp:ignition_system	hypergolic
gptkbp:investment	60 atm
gptkbp:mission	gptkb:Apollo_program
gptkbp:number_of_engines	gptkb:5
gptkbp:number_of_rooms	single chamber 70 atm
gptkbp:oxidation_states	liquid oxygen
gptkbp:produces	15 engines
gptkbp:propulsion	1,500,000 lbf 81:1
gptkbp:specific_impulse	263 seconds
gptkbp:successor	gptkb:F-1_B
gptkbp:used_in	gptkb:Saturn_V
gptkbp:water_requirement	12,000 lb/min 29,000 lb/min
gptkbp:weight	18,500 lb
gptkbp:bfsParent	gptkb:Saturn_V gptkb:NASA_Stennis_Space_Center gptkb:Rocketdyne
gptkbp:bfsLayer	4