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gptkbp:instance_of
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gptkb:spacecraft
|
|
gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Apollo_command_module
|
|
gptkbp:contains
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gptkb:aircraft
environmental control system
power distribution system
reaction control system
storage for supplies
service propulsion system
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|
gptkbp:crew
|
gptkb:3
|
|
gptkbp:designed_by
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gptkb:NASA
|
|
gptkbp:developed_by
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gptkb:North_American_Aviation
|
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gptkbp:diameter
|
4.2 m
|
|
gptkbp:first_flight
|
gptkb:Apollo_17
gptkb:Apollo_7
|
|
gptkbp:has_method
|
gptkb:United_States_Coast_Guard_Cutter
gptkb:rocket
gptkb:computer
gptkb:Telecommunications_company
thermal control system
guidance and navigation system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Apollo service module
|
|
gptkbp:influenced_by
|
gptkb:spacecraft
gptkb:Gemini_spacecraft
|
|
gptkbp:is_designed_for
|
crew safety
|
|
gptkbp:is_equipped_with
|
solar panels
backup systems
reaction control thrusters
main engine
|
|
gptkbp:is_part_of
|
gptkb:Apollo_lunar_missions
|
|
gptkbp:is_tested_for
|
Earth's atmosphere
vacuum conditions
thermal vacuum tests
simulated lunar conditions
vibration tests
high-altitude conditions
acoustic tests
electromagnetic interference tests
shock tests
|
|
gptkbp:is_used_for
|
lunar missions
Earth orbit missions
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
10,000 kg
|
|
gptkbp:length
|
6.9 m
|
|
gptkbp:manufacturer
|
gptkb:North_American_Rockwell
|
|
gptkbp:operational_area
|
1966-1972
|
|
gptkbp:part_of
|
gptkb:software
|
|
gptkbp:power_output
|
fuel cells
|
|
gptkbp:primary_function
|
support crew and systems
|
|
gptkbp:replaced_by
|
gptkb:Orion_service_module
|
|
gptkbp:retired
|
gptkb:1972
|
|
gptkbp:speed
|
gptkb:battle
|
|
gptkbp:successor
|
gptkb:Orion_spacecraft
|
|
gptkbp:used_in
|
gptkb:Apollo_14
gptkb:Apollo_10
gptkb:Apollo_16
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_7
gptkb:Apollo_9
gptkb:Apollo_11
gptkb:Apollo_13
gptkb:Apollo_12
gptkb:Apollo_1
|