S-IVC

GPTKB entity

Statements (56)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:associated_with gptkb:NASA's_Apollo_program
gptkbp:built gptkb:15
gptkbp:check_in_time 150 seconds
gptkbp:crew_capacity gptkb:3
gptkbp:debut Apollo 4 to Apollo 17
gptkbp:design_purpose Lunar missions
gptkbp:designed_by gptkb:NASA
gptkbp:development_cost $1 billion
gptkbp:diameter 4.0 meters
gptkbp:engine_configuration clustered engines
gptkbp:engine_type gptkb:F-1_engine
gptkbp:first_flight gptkb:1967
gptkb:1975
gptkb:Apollo_4
gptkbp:fuel_capacity 150,000 liters
gptkbp:fuel_type kerosene
gptkbp:function gptkb:gasoline
gptkbp:height 10.1 meters
gptkbp:historical_impact enabled moon landings
https://www.w3.org/2000/01/rdf-schema#label S-IVC
gptkbp:influenced future rocket designs
gptkbp:influenced_by gptkb:Juno_II
gptkbp:inspiration gptkb:Apollo_Lunar_Program
gptkbp:launch_mass 2,800,000 kg
gptkbp:launch_site gptkb:Kennedy_Space_Center
gptkbp:launch_vehicle gptkb:Saturn_V
gptkbp:launched gptkb:15
gptkb:Launch_Complex_39
gptkbp:legacy pioneered heavy-lift launch vehicles
gptkbp:manufacturer gptkb:North_American_Aviation
gptkbp:mass 25,000 kg
gptkbp:mission gptkb:Apollo-Soyuz_Test_Project
gptkbp:mission_duration 8 days
gptkbp:mission_type crewed missions
gptkbp:notable_feature five F-1 engines
gptkbp:number_of_engines gptkb:5
gptkbp:number_of_stages gptkb:Saturn_V
gptkb:S-IVB
gptkbp:operational_period 1967-1975
gptkbp:operational_status retired
gptkbp:operational_use gptkb:Apollo_program
gptkbp:oxidation_states liquid oxygen
gptkbp:oxidizer_capacity 200,000 liters
gptkbp:propulsion gptkb:RP-1
liquid oxygen
1,000 k N
gptkbp:related_to gptkb:Saturn_I
gptkbp:replaced_by gptkb:S-IVB
gptkbp:role gptkb:first_stage
gptkbp:significance first stage of Saturn V
gptkbp:specification advanced rocket technology
gptkbp:successor gptkb:S-IVB
gptkbp:used_in gptkb:Saturn_V
gptkbp:bfsParent gptkb:S-IVB
gptkbp:bfsLayer 5