gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:contains
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gptkb:Environmental_Protection_Agency
gptkb:Service_Propulsion_System
gptkb:communication_systems
Electrical Power System
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gptkbp:control_system
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gptkb:Inertial_Navigation_System
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gptkbp:cooling_system
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Radiator system
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gptkbp:crew_capacity
|
3 astronauts
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gptkbp:designed_by
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gptkb:North_American_Aviation
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gptkbp:diameter
|
4.2 m
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gptkbp:first_introduced
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gptkb:Apollo_7
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gptkbp:fuel_type
|
Hypergolic propellant
|
https://www.w3.org/2000/01/rdf-schema#label
|
Apollo Service Module
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gptkbp:is_capable_of
|
supporting a crew of three
|
gptkbp:is_designed_for
|
deep space missions
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gptkbp:is_designed_to
|
ensure mission success
enable lunar exploration
return safely to Earth
withstand re-entry heat
be jettisoned before re-entry
facilitate crew safety
support scientific experiments
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gptkbp:is_equipped_with
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Solar panels
Battery systems
Navigation aids
Guidance system
Waste management system
Thermal control systems
Structural framework
Oxygen system
Telemetry system
Emergency systems
Communication antennas
Water recovery system
RCS thrusters
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gptkbp:is_part_of
|
gptkb:Apollo_Lunar_Module
gptkb:Apollo_program
|
gptkbp:is_used_for
|
lunar missions
|
gptkbp:is_used_to
|
transport astronauts
provide life support during missions
provide power to the Command Module
provide propulsion for the mission
support lunar landings
|
gptkbp:launched
|
gptkb:Saturn_V_rocket
|
gptkbp:launched_in
|
gptkb:Kennedy_Space_Center
|
gptkbp:length
|
6.9 m
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gptkbp:manufacturer
|
gptkb:Rockwell_International
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gptkbp:mass
|
4,500 kg
|
gptkbp:operational_period
|
1967-1972
|
gptkbp:part_of
|
gptkb:Apollo_program
|
gptkbp:provides
|
gptkb:power
propulsion
communications
life support
|
gptkbp:retired
|
gptkb:1972
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gptkbp:storage
|
Consumables storage
|
gptkbp:succeeded_by
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gptkb:Orion_spacecraft
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gptkbp:used_in
|
gptkb:Apollo_17
gptkb:Apollo_missions
|
gptkbp:bfsParent
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gptkb:Apollo_11_Command_Module
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gptkbp:bfsLayer
|
4
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