|
gptkbp:instance_of
|
gptkb:Space_Launch_System
gptkb:Team_Rocket
|
|
gptkbp:assembly_location
|
gptkb:NASA's_Vehicle_Assembly_Building
|
|
gptkbp:check_in_time
|
6 minutes
2.5 minutes
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:cultural_impact
|
Featured in films and documentaries
Symbol of the Space Race
Inspiration for STEM education
|
|
gptkbp:debut
|
gptkb:Apollo_17
November 9, 1967
|
|
gptkbp:decommissioned
|
gptkb:1973
|
|
gptkbp:design
|
gptkb:Wernher_von_Braun
|
|
gptkbp:designated_as
|
gptkb:AS-504
gptkb:AS-506
gptkb:AS-509
gptkb:AS-511
gptkb:AS-513
gptkb:AS-514
gptkb:AS-515
AS-503
AS-505
AS-507
AS-508
AS-510
AS-512
AS-516
AS-517
AS-518
AS-519
AS-520
AS-521
AS-522
AS-523
AS-524
AS-525
AS-526
AS-527
AS-528
AS-529
AS-530
AS-531
AS-532
AS-533
AS-534
AS-535
AS-536
AS-537
AS-538
AS-539
AS-540
AS-541
AS-542
AS-543
AS-544
AS-545
AS-546
AS-547
AS-548
AS-549
AS-550
AS-551
AS-552
AS-553
AS-554
AS-555
AS-556
AS-557
AS-558
AS-559
AS-560
AS-561
AS-562
AS-563
AS-564
AS-565
AS-566
AS-567
AS-568
AS-569
AS-570
AS-571
AS-572
AS-573
AS-574
AS-575
AS-576
AS-577
AS-578
AS-579
AS-580
AS-581
AS-582
AS-583
AS-584
AS-585
AS-586
AS-587
AS-588
AS-589
AS-590
AS-591
AS-592
AS-593
AS-594
AS-595
AS-596
AS-597
AS-598
AS-599
AS-600
|
|
gptkbp:designed_by
|
gptkb:Wernher_von_Braun
gptkb:NASA
|
|
gptkbp:designed_for
|
gptkb:human_spaceflight
|
|
gptkbp:developed_by
|
gptkb:North_American_Aviation
gptkb:NASA
|
|
gptkbp:engine
|
gptkb:1
gptkb:5
2
|
|
gptkbp:engine_type
|
gptkb:Rocketdyne_F-1
gptkb:F-1
gptkb:F-1_engine
gptkb:J-2
|
|
gptkbp:first_flight
|
gptkb:1967
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_4
November 9, 1967
1967-11-09
successful
1973-05-14
1975-07-15
1967-10-27
|
|
gptkbp:first_launch_mission
|
gptkb:Apollo_4
|
|
gptkbp:first_stage_diameter
|
33 feet
|
|
gptkbp:first_stage_separation
|
42 miles altitude
|
|
gptkbp:flight_style
|
gptkb:13
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
Liquid Hydrogen and Liquid Oxygen
|
|
gptkbp:height
|
111 m
111 meters
363 feet
110.6 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Saturn V
|
|
gptkbp:influenced_by
|
gptkb:Vostok_rocket
gptkb:Soyuz_spacecraft
gptkb:German_V-2_rocket
gptkb:Ariane_rocket
gptkb:Titan_rocket
gptkb:Electron_rocket
gptkb:Atlas_rocket
gptkb:Saturn_I
gptkb:Delta_rocket
gptkb:Falcon_rocket
gptkb:Redstone_rocket
|
|
gptkbp:inspiration
|
gptkb:Long_March_5
gptkb:Ares_I
gptkb:Ariane_5
gptkb:Delta_IV_Heavy
gptkb:Space_Launch_System
gptkb:Falcon_Heavy
gptkb:Space_Shuttle
Von Braun's designs
|
|
gptkbp:inspired
|
future rocket designs
|
|
gptkbp:is_a
|
gptkb:Space_Launch_System
|
|
gptkbp:is_known_for
|
its height and power
|
|
gptkbp:is_part_of
|
gptkb:Saturn_rocket_family
|
|
gptkbp:launch_date
|
December 7, 1972
November 9, 1967
May 14, 1973
|
|
gptkbp:launch_mass
|
2,800,000 kg
2,800,000 pounds
|
|
gptkbp:launch_price
|
$1 billion
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Air_Force_Station
|
|
gptkbp:launch_vehicle
|
heavy-lift launch vehicle
|
|
gptkbp:launch_window
|
1967-1972
|
|
gptkbp:launched
|
gptkb:13
gptkb:Launch_Complex_39_A
gptkb:Launch_Complex_39_B
|
|
gptkbp:legacy
|
gptkb:space_exploration
Paved the way for future space exploration
most powerful rocket ever built
Enabled human moon landing
|
|
gptkbp:manufacturer
|
gptkb:Douglas_Aircraft_Company
gptkb:IBM
gptkb:Boeing
gptkb:Rocketdyne
gptkb:North_American_Aviation
gptkb:NASA
|
|
gptkbp:mass
|
2,800,000 kg
2.8 million pounds
2,800,000 pounds
3,000,000 pounds
|
|
gptkbp:maximum_payload_to_leo
|
140,000 kg
|
|
gptkbp:maximum_payload_to_moon
|
48,600 kg
|
|
gptkbp:mission
|
gptkb:Skylab
gptkb:Apollo_16
gptkb:Skylab_program
gptkb:Apollo_program
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_11
gptkb:Skylab_2
gptkb:Apollo-Soyuz_Test_Project
|
|
gptkbp:notable_feature
|
first rocket to send humans to the Moon
largest rocket ever built
first rocket to achieve a lunar landing
first rocket to achieve a lunar orbit
first rocket to achieve a lunar return
most powerful rocket ever launched
first rocket to launch a spacecraft to another celestial body
|
|
gptkbp:notable_launches
|
gptkb:Apollo_16
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_11
|
|
gptkbp:notable_mission
|
gptkb:Apollo_10
gptkb:Apollo_16
gptkb:Apollo_6
gptkb:Skylab_3
gptkb:Skylab_4
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_7
gptkb:Apollo_9
gptkb:Apollo_11
gptkb:Apollo_13
gptkb:Skylab_2
gptkb:Apollo-Soyuz_Test_Project
gptkb:Apollo_4
|
|
gptkbp:number_of_engines
|
gptkb:5
1 on S-IVB
5 on S-IC
5 on S-II
|
|
gptkbp:number_of_stages
|
gptkb:F-1_engines
gptkb:J-2_engines
gptkb:3
gptkb:S-IVB
gptkb:F-1
gptkb:J-2
gptkb:J-2_engine
gptkb:S-IC
gptkb:S-II
200,000 pounds
7.5 million pounds
1,000 k N
1.1 million pounds
34,000 k N
5,000 k N
|
|
gptkbp:operated_by
|
gptkb:NASA
|
|
gptkbp:operational_period
|
1967-1975
1967-1973
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:part_of
|
gptkb:Saturn_launch_vehicle_family
|
|
gptkbp:payload_capacity
|
140,000 kg
140,000 pounds
310,000 pounds
140,000 kg to Low Earth Orbit
310,000 pounds to Low Earth Orbit
140,000 kg to LEO
|
|
gptkbp:payload_capacity_translunar_injection
|
48,600 kg
94,000 pounds
|
|
gptkbp:payload_to_tli
|
48,600 kg
|
|
gptkbp:propulsion
|
7.5 million pounds
|
|
gptkbp:record
|
most powerful rocket ever built
Longest operational period for a rocket of its size
Highest payload capacity to LEO
Most powerful launch vehicle ever
Most successful launch vehicle in history
|
|
gptkbp:replaced_by
|
gptkb:Space_Shuttle
|
|
gptkbp:retired
|
gptkb:1973
gptkb:1975
|
|
gptkbp:retirement_year
|
gptkb:1973
|
|
gptkbp:second_stage_diameter
|
33 feet
|
|
gptkbp:second_stage_separation
|
115 miles altitude
|
|
gptkbp:significance
|
moon landing missions
Largest and most powerful rocket ever built
Largest and most powerful rocket ever built.
|
|
gptkbp:strategic_goals
|
gptkb:0
|
|
gptkbp:success
|
gptkb:13
|
|
gptkbp:success_rate
|
100%
100% for crewed missions
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:system
|
gptkb:Skylab_program
gptkb:Apollo_program
|
|
gptkbp:third_stage_burn_time
|
2.5 minutes
|
|
gptkbp:third_stage_diameter
|
20 feet
|
|
gptkbp:third_stage_separation
|
185 miles altitude
|
|
gptkbp:total_failures
|
gptkb:0
|
|
gptkbp:total_successes
|
gptkb:13
|
|
gptkbp:total_thrust
|
7.5 million pounds
|
|
gptkbp:type
|
gptkb:Space_Launch_System
|
|
gptkbp:used_for
|
gptkb:Skylab_program
gptkb:Apollo_Moon_missions
gptkb:Apollo_program
gptkb:Apollo_missions
Lunar missions
|
|
gptkbp:used_for_crewed_lunar_missions
|
yes
|
|
gptkbp:used_for_uncrewed_missions
|
yes
|
|
gptkbp:used_in
|
gptkb:Skylab_program
gptkb:Apollo_program
gptkb:Apollo_missions
gptkb:Apollo-Soyuz_Test_Project
gptkb:Project_Apollo-Saturn
|
|
gptkbp:weight
|
3,000,000 pounds
|
|
gptkbp:bfsParent
|
gptkb:Wernher_von_Braun
gptkb:NASA
|
|
gptkbp:bfsLayer
|
3
|