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gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:academic_programs
|
comprised of leading aerospace engineers
|
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gptkbp:associated_missions
|
Apollo 8, Apollo 10, Apollo 11, Apollo 12, Apollo 14, Apollo 15, Apollo 16, Apollo 17
|
|
gptkbp:can_be_configured_for
|
multiple payloads
|
|
gptkbp:challenges
|
overcome during development
|
|
gptkbp:check_in_time
|
approximately 5 minutes
2.5 minutes
|
|
gptkbp:commemorated_by
|
gptkb:museums
|
|
gptkbp:conducts_research_on
|
rocket propulsion systems
|
|
gptkbp:control_system
|
gptkb:sensors
inertial guidance system
|
|
gptkbp:crew
|
enabled crewed lunar landings
|
|
gptkbp:debut
|
part of the most powerful rocket ever built
|
|
gptkbp:decommissioned
|
gptkb:1973
after Apollo program
|
|
gptkbp:design_features
|
advanced for its time
|
|
gptkbp:design_purpose
|
to propel spacecraft to the Moon
|
|
gptkbp:designed_by
|
gptkb:Douglas_Aircraft_Company
|
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gptkbp:developed_by
|
gptkb:NASA
|
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gptkbp:development
|
developed in the 1960s
|
|
gptkbp:diameter
|
4.2 meters
4.0 meters
21.7 feet
|
|
gptkbp:dimensions
|
10.1 meters in length
|
|
gptkbp:economic_impact
|
led to advancements in rocket technology
|
|
gptkbp:elevation
|
low Earth orbit
|
|
gptkbp:engine_configuration
|
single engine configuration
|
|
gptkbp:engine_type
|
gptkb:J-2_engine
|
|
gptkbp:exhibition
|
space museums
|
|
gptkbp:first_flight
|
gptkb:Apollo_17
gptkb:Apollo_8
|
|
gptkbp:first_introduced
|
gptkb:Apollo_8
|
|
gptkbp:fuel_economy
|
optimized for lunar missions
|
|
gptkbp:fuel_tank_design
|
cryogenic tank design
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:function
|
gptkb:third_stage_of_Saturn_V
propulsion
|
|
gptkbp:has_ability
|
contributed to successful Apollo missions
|
|
gptkbp:has_function
|
third stage
|
|
gptkbp:height
|
18.3 meters
|
|
gptkbp:historical_event
|
gptkb:space_exploration
|
|
gptkbp:historical_significance
|
first stage to achieve lunar orbit
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
S-IVB
|
|
gptkbp:ignition_system
|
start sequence initiated by ground control
|
|
gptkbp:influence
|
on modern space exploration
|
|
gptkbp:instrument
|
telemetry systems
|
|
gptkbp:is_associated_with
|
gptkb:Lunar_Module
gptkb:Apollo_13_mission
|
|
gptkbp:is_capable_of
|
placing payloads into orbit
|
|
gptkbp:is_celebrated_for
|
its engineering achievements
|
|
gptkbp:is_celebrated_in
|
space exploration history.
anniversaries of Apollo missions
|
|
gptkbp:is_critical_for
|
Lunar landing
|
|
gptkbp:is_designed_for
|
crew missions
|
|
gptkbp:is_designed_to
|
achieve escape velocity
|
|
gptkbp:is_documented_in
|
NASA archives
|
|
gptkbp:is_equipped_with
|
fuel tanks
|
|
gptkbp:is_featured_in
|
documentaries about space travel
|
|
gptkbp:is_fired_during
|
translunar phase
|
|
gptkbp:is_followed_by
|
gptkb:S-IVC
|
|
gptkbp:is_followed_by_burn
|
Earth orbit insertion
|
|
gptkbp:is_influential_in
|
rocket design
|
|
gptkbp:is_integrated_with
|
gptkb:S-II_stage
|
|
gptkbp:is_linked_to
|
gptkb:Apollo_Lunar_Module
gptkb:human_spaceflight
|
|
gptkbp:is_notable_for
|
its reliability
|
|
gptkbp:is_noted_for
|
its innovative technology
|
|
gptkbp:is_part_of
|
gptkb:Apollo_program
|
|
gptkbp:is_part_of_design
|
Saturn V architecture
|
|
gptkbp:is_part_of_launch
|
gptkb:Apollo_11
|
|
gptkbp:is_recognized_as
|
one of the most powerful stages
|
|
gptkbp:is_recognized_by
|
NASA historians
|
|
gptkbp:is_referenced_in
|
gptkb:literature
|
|
gptkbp:is_retrofitted_for
|
future missions
|
|
gptkbp:is_studied_in
|
aerospace engineering courses
|
|
gptkbp:is_subject_to
|
extensive testing
|
|
gptkbp:is_tested_for
|
gptkb:Marshall_Space_Flight_Center
safety protocols
static fire tests
conducted at Marshall Space Flight Center
extensive pre-flight testing conducted
|
|
gptkbp:is_used_for
|
translunar injection
|
|
gptkbp:is_used_for_mission
|
gptkb:Apollo_17
|
|
gptkbp:is_used_in
|
Skylab missions
|
|
gptkbp:is_utilized_in
|
gptkb:Space_Shuttle
|
|
gptkbp:launch_mass
|
130,000 kg
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
|
|
gptkbp:launched_in
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:legacy
|
gptkb:Saturn_V_program
influenced future rocket designs
|
|
gptkbp:length
|
58.6 feet
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:mass
|
30,000 pounds
|
|
gptkbp:mission
|
gptkb:Apollo_15
Apollo 17 in December 1972
remained in orbit or impacted the Moon
transit to lunar orbit
|
|
gptkbp:mission_duration
|
varied by mission
|
|
gptkbp:mission_type
|
crewed and uncrewed missions
|
|
gptkbp:number_built
|
gptkb:15
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operated_by
|
gptkb:J-2_engine
|
|
gptkbp:operational_period
|
1967-1972
approximately 2.5 minutes
|
|
gptkbp:operational_use
|
final stage of Saturn V
|
|
gptkbp:orbital_altitude
|
Earth orbit
performed after S-II stage
|
|
gptkbp:part_of
|
gptkb:Saturn_V
|
|
gptkbp:payload_capacity
|
up to 45,000 kg to low Earth orbit
|
|
gptkbp:performance
|
highly reliable
|
|
gptkbp:preceded_by
|
gptkb:S-II
|
|
gptkbp:predecessor
|
gptkb:S-IV
|
|
gptkbp:project
|
managed by NASA
|
|
gptkbp:propulsion
|
liquid hydrogen and liquid oxygen
200,000 pounds
6.67:1
|
|
gptkbp:replaced_by
|
gptkb:S-IVC
|
|
gptkbp:retired
|
gptkb:1975
|
|
gptkbp:reused_in
|
multiple Apollo missions
|
|
gptkbp:significance
|
critical for lunar missions
|
|
gptkbp:specification
|
detailed in NASA documentation
|
|
gptkbp:staging_event
|
separation from S-II
|
|
gptkbp:successor
|
gptkb:S-IVC
|
|
gptkbp:system
|
gptkb:Space_Launch_System
|
|
gptkbp:used_by
|
gptkb:NASA
|
|
gptkbp:used_for
|
translunar injection
|
|
gptkbp:used_in
|
gptkb:Apollo_program
|
|
gptkbp:weight
|
approximately 30,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Saturn_V
gptkb:Saturn_V_rocket
|
|
gptkbp:bfsLayer
|
4
|