F-1 engines

GPTKB entity

Statements (55)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:aircraft_operated gptkb:Saturn_I
gptkbp:check_in_time 150 seconds
gptkbp:combustor_type gas-generator cycle
gptkbp:cooling_system regenerative cooling
gptkbp:designed_by gptkb:Rocketdyne
gptkbp:development gptkb:1955
gptkbp:engine gptkb:space_exploration
gptkb:Apollo_missions
gptkb:Rocketdyne
gptkb:NASA
gptkb:Team_Rocket
gptkb:historical_significance
aerospace engineering
manned spaceflight
open cycle
liquid propulsion
reliability issues
gptkbp:engine_configuration high performance
single-chamber
single-chamber engine
gptkbp:engine_cost high development cost
gptkbp:engine_power gptkb:1975
high thrust
gptkbp:engine_reusability not reusable
gptkbp:engine_success gptkb:Apollo_11_mission
gptkbp:engine_type liquid-fueled
gptkbp:exhaust_system bell nozzle
gptkbp:first_flight gptkb:1967
gptkb:1975
gptkbp:fuel_capacity 12.2 feet
19.5 feet
gptkbp:fuel_type gptkb:RP-1
https://www.w3.org/2000/01/rdf-schema#label F-1 engines
gptkbp:ignition_system hypergolic
gptkbp:impact moon landing missions
gptkbp:investment 50 psi
gptkbp:is_tested_for static fire tests
gptkbp:mission gptkb:Apollo_program
gptkbp:number_of_engines gptkb:5
gptkbp:number_of_rooms one
gptkbp:oxidation_states liquid oxygen
gptkbp:produces gptkb:15
gptkbp:propulsion 8.1
1,500,000 lbf
1.5 million pounds
gptkbp:specific_impulse 263 seconds
gptkbp:successor gptkb:F-1_B
gptkbp:used_in gptkb:Saturn_V
gptkbp:used_in_rocket gptkb:Saturn_V_rocket
gptkbp:water_requirement 12,000 pounds per minute
29,000 pounds per minute
gptkbp:weight 18,500 pounds
gptkbp:bfsParent gptkb:Saturn_V
gptkbp:bfsLayer 4