F-1 rocket engine

GPTKB entity

Statements (52)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:application gptkb:Apollo_program
gptkbp:check_in_time 150 seconds
gptkbp:combustor_type Gas-generator cycle
gptkbp:control_system gptkb:manual
gptkbp:cooling_system regenerative cooling
gptkbp:debut gptkb:1965
gptkbp:designed_by gptkb:Rocketdyne
gptkbp:development 1955-1967
gptkbp:diameter 12.2 ft
gptkbp:engine gptkb:advanced_technology
modular
historic significance
open cycle
shutdown sequence
NASA collaboration
gptkbp:engine_configuration detailed design
vertical
gptkbp:engine_power high performance
high reliability
gptkbp:engine_startup start sequence
gptkbp:engine_type liquid-fueled
F-1 A, F-1 B
gptkbp:exhaust_system bell nozzle
gptkbp:facilities Rocketdyne test facility
gptkbp:first_flight gptkb:1967
gptkbp:fuel_type RP-1 and Liquid Oxygen
turbopump
https://www.w3.org/2000/01/rdf-schema#label F-1 rocket engine
gptkbp:ignition_system Hypergolic
gptkbp:impact gptkb:space_exploration
gptkbp:is_tested_for static fire tests
gptkbp:launch_vehicle gptkb:Saturn_I
gptkbp:length 19.5 ft
gptkbp:maintenance periodic checks
gptkbp:number_of_engines gptkb:5
gptkbp:number_of_rooms single chamber
70 psi
gptkbp:operational_status retired
gptkbp:oxidizer_pump_type turbopump
gptkbp:produces gptkb:15
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:National_Air_and_Space_Museum
gptkb:Smithsonian_National_Air_and_Space_Museum
gptkbp:bfsLayer 3