|
gptkbp:instance_of
|
gptkb:Space_Launch_System
gptkb:Team_Rocket
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:diameter
|
3.05 meters
10.1 meters
|
|
gptkbp:engine_type
|
gptkb:Rocketdyne_J-2
gptkb:F-1
gptkb:F-1_engine
gptkb:J-2_engine
|
|
gptkbp:first_flight
|
1966-10-28
1975-07-15
1966-01-29
1966-02-26
1966-10-29
|
|
gptkbp:flight_style
|
gptkb:9
gptkb:17
|
|
gptkbp:height
|
34.6 meters
67.1 m
36.2 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Saturn IB
|
|
gptkbp:is_part_of
|
gptkb:Saturn_rocket_family
|
|
gptkbp:launch_mass
|
120,000 kg
118,000 kg
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launched
|
gptkb:10
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
gptkb:NASA
|
|
gptkbp:mass
|
120,000 kg
|
|
gptkbp:mission
|
gptkb:Skylab_program
gptkb:Apollo_program
|
|
gptkbp:notable_mission
|
gptkb:Apollo_15
gptkb:Apollo_7
|
|
gptkbp:number_of_engines
|
8
|
|
gptkbp:number_of_stages
|
gptkb:F-1_engines
gptkb:H-1_engines
gptkb:J-2_engine
2
|
|
gptkbp:operational_status
|
1966 to 1975
|
|
gptkbp:part_of
|
gptkb:Saturn_launch_vehicle_family
|
|
gptkbp:payload_capacity
|
22,000 kg
22,000 kg to LEO
22,700 kg
|
|
gptkbp:payload_capacity_translunar_injection
|
9,000 kg
|
|
gptkbp:strategic_goals
|
gptkb:0
|
|
gptkbp:success
|
gptkb:9
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:successor
|
gptkb:Saturn_V
|
|
gptkbp:used_for
|
gptkb:Apollo_Lunar_Module_Test_Flight
gptkb:Apollo_program
gptkb:Apollo_missions
|
|
gptkbp:bfsParent
|
gptkb:Skylab
gptkb:KSC_Launch_Complex_33
gptkb:KSC_Launch_Complex_66
gptkb:Apollo-Soyuz_Test_Project
|
|
gptkbp:bfsLayer
|
4
|