|
gptkbp:instance_of
|
gptkb:Command_Line_Interface
|
|
gptkbp:communication_system
|
S-band radio
|
|
gptkbp:control_system
|
manual and automatic
|
|
gptkbp:cooling_system
|
ablative material
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:designed_by
|
gptkb:Boeing
|
|
gptkbp:diameter
|
13 feet
|
|
gptkbp:first_flight
|
gptkb:Apollo_17
gptkb:Apollo_1
|
|
gptkbp:function
|
crew transport
|
|
gptkbp:height
|
11 feet
|
|
gptkbp:historical_significance
|
first crewed spacecraft to orbit the Moon
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing-built Command Module
|
|
gptkbp:influenced_by
|
gptkb:Apollo_Lunar_Module
gptkb:spacecraft
gptkb:Soyuz_spacecraft
gptkb:Gemini_spacecraft
|
|
gptkbp:inspiration
|
future spacecraft designs
|
|
gptkbp:key_feature
|
gptkb:navigation_system
gptkb:Command_Line_Interface
gptkb:Public_service
gptkb:scientific_instruments
gptkb:launch_escape_system
modular design
crew accommodations
redundant systems
thermal protection system
parachute recovery system
high altitude performance
three-module design
emergency systems
long duration missions
reentry capability
stability during reentry
|
|
gptkbp:landing_distance
|
splashdown
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
|
|
gptkbp:life_support_system
|
environmental control system
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:material
|
aluminum alloy
|
|
gptkbp:mission_duration
|
up to 14 days
|
|
gptkbp:notable_mission
|
gptkb:Apollo_14
gptkb:Apollo_16
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_11
gptkb:Apollo_13
gptkb:Apollo_12
|
|
gptkbp:operational_period
|
1967 to 1972
|
|
gptkbp:power_source
|
fuel cells
|
|
gptkbp:recovery_method
|
gptkb:naval_warfare
|
|
gptkbp:success_rate
|
100% for crewed missions
|
|
gptkbp:successor
|
gptkb:Orion_spacecraft
|
|
gptkbp:used_in
|
gptkb:Apollo_program
|
|
gptkbp:weight
|
5,000 pounds
|
|
gptkbp:bfsParent
|
gptkb:Apollo_7
|
|
gptkbp:bfsLayer
|
5
|