Saturn I

GPTKB entity

Statements (125)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkb:rocket
gptkbp:associated_with gptkb:NASA_Marshall_Space_Flight_Center
gptkbp:crew gptkb:0
gptkbp:debut_year 1975-07-15
1961-10-27
gptkbp:designated_as SA-1 to SA-10
gptkbp:developer 1955-1961
gptkbp:diameter 3.05 meters
6.6 meters
gptkbp:engine_type gptkb:Rocketdyne_F-1
gptkb:Rocketdyne_H-1
gptkb:H-1_engine
gptkbp:first_flight gptkb:SA-10
gptkb:10
8
1965-11-09
1965-11-14
1961-10-27
1965-11-28
SA-1
gptkbp:fuel_type gptkb:RP-1/_LOX
L H2/ LOX
gptkbp:height 25.6 m
25.6 meters
61.6 m
gptkbp:historical_significance paved the way for crewed spaceflight
https://www.w3.org/2000/01/rdf-schema#label Saturn I
gptkbp:influenced future launch vehicles
gptkbp:influenced_by gptkb:Redstone_rocket
gptkbp:inspiration gptkb:Saturn_V
gptkbp:is_part_of gptkb:Saturn_rocket_family
gptkbp:is_tested_for gptkb:software
gptkbp:is_used_for gptkb:Project_Gemini
gptkb:software
gptkbp:launch_site gptkb:cape
gptkbp:launch_vehicle 150,000 kg
two-stage
heavy lift
Saturn family
gptkbp:launched gptkb:10
gptkb:Launch_Complex_37
8
gptkbp:legacy foundation for future Saturn rockets
gptkbp:manufacturer gptkb:CEO
gptkb:NASA
gptkbp:mission gptkb:Apollo_14
gptkb:Apollo_10
gptkb:Apollo_16
gptkb:Apollo_6
gptkb:Apollo_19
gptkb:Apollo_20
gptkb:Apollo_21
gptkb:Apollo_22
gptkb:Apollo_23
gptkb:Apollo_24
gptkb:Apollo_25
gptkb:Apollo_26
gptkb:Apollo_27
gptkb:Apollo_28
gptkb:Apollo_29
gptkb:Apollo_31
gptkb:Apollo_32
gptkb:Apollo_34
gptkb:Apollo_36
gptkb:Apollo_37
gptkb:Apollo_38
gptkb:Apollo_39
gptkb:Apollo_40
gptkb:Apollo_41
gptkb:Apollo_43
gptkb:Apollo_46
gptkb:Apollo_49
gptkb:Apollo_50
gptkb:Skylab_3
gptkb:Skylab_4
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_7
gptkb:Apollo_9
gptkb:Apollo_18
gptkb:Apollo_11
gptkb:Apollo_13
gptkb:Skylab_2
gptkb:Apollo_12
gptkb:Apollo-Soyuz_Test_Project
gptkb:Gemini_8
gptkb:Apollo_4
gptkb:Apollo_1
orbital
Apollo 30
Apollo 33
Apollo 35
Apollo 42
Apollo 44
Apollo 45
Apollo 47
Apollo 48
gptkbp:notable_album Apollo 4 test flight
gptkbp:number_of_stages gptkb:S-IV
gptkb:H-1_engines
gptkb:Juno_I
gptkb:Juno_II
2
S-IB
1,500 k N
75 k N
gptkbp:operational_area 1961-1965
gptkbp:operational_status retired
gptkbp:part_of gptkb:Saturn_launch_vehicle_family
gptkbp:replaced_by gptkb:Saturn_IB
gptkbp:seating_capacity 4,500 kg
8,000 kg
22,000 kg to LEO
4,000 kg to Low Earth Orbit
4,500 kg to LEO
gptkbp:significant_event first successful launch of a Saturn rocket
gptkbp:strategic_importance 2
gptkbp:succeeded_by 100%
8
gptkbp:successor gptkb:Saturn_IB
gptkbp:used_in gptkb:early_Apollo_missions
gptkbp:bfsParent gptkb:Saturn_V
gptkbp:bfsLayer 3