|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:combustor_type
|
gas-generator cycle
|
|
gptkbp:control_system
|
gimbaled thrust
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:cultural_impact
|
symbol of space exploration
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
33 feet
|
|
gptkbp:documentary
|
gptkb:Apollo_11
gptkb:The_Last_Man_on_the_Moon
|
|
gptkbp:engine
|
1955-1967
|
|
gptkbp:engine_configuration
|
single combustion chamber
F-1 specifications
|
|
gptkbp:engine_test_stand
|
gptkb:B-2_Test_Stand
|
|
gptkbp:engine_type
|
gptkb:F-1_engine
|
|
gptkbp:exhaust_system
|
2630 m/s
|
|
gptkbp:first_flight
|
November 9, 1967
July 16, 1975
|
|
gptkbp:flight_style
|
gptkb:13
|
|
gptkbp:fuel_capacity
|
12.2 feet
19.7 feet
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
gptkbp:height
|
363 feet
|
|
gptkbp:historical_significance
|
first rocket to send humans to the Moon
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Saturn V rocket engine
|
|
gptkbp:ignition_system
|
hypergolic ignition
|
|
gptkbp:influenced_by
|
gptkb:V-2_rocket
|
|
gptkbp:inspiration
|
Von Braun's designs
|
|
gptkbp:investment
|
50 psi
|
|
gptkbp:involved_technology
|
liquid rocket propulsion
thrust vector control
cryogenic propellants
engine testing protocols
rocket staging
|
|
gptkbp:is_tested_for
|
gptkb:Marshall_Space_Flight_Center
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Air_Force_Station
|
|
gptkbp:legacy
|
influenced future rocket designs
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:notable_mission
|
gptkb:Skylab
gptkb:Apollo_17
gptkb:Apollo_11
gptkb:Apollo-Soyuz_Test_Project
|
|
gptkbp:number_of_engines
|
gptkb:5
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_period
|
1967-1975
|
|
gptkbp:payload_capacity
|
140,000 kg to low Earth orbit
|
|
gptkbp:propulsion
|
7.5 million pounds
|
|
gptkbp:retirement_year
|
gptkb:1975
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:used_in
|
gptkb:Apollo_program
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:the_James_S._Mc_Donnell_Space_Hangar
|
|
gptkbp:bfsLayer
|
5
|