|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:aftermath
|
gptkb:Apollo_17
|
|
gptkbp:challenges
|
reentry heating
|
|
gptkbp:communication
|
gptkb:aircraft
|
|
gptkbp:controls
|
manual and automatic
|
|
gptkbp:cooling_system
|
ablative material
insulation blankets
|
|
gptkbp:crew
|
gptkb:aircraft
gptkb:3
gptkb:Buzz_Aldrin
gptkb:Michael_Collins
gptkb:Neil_Armstrong
|
|
gptkbp:cultural_impact
|
iconic status
|
|
gptkbp:designed_by
|
gptkb:North_American_Aviation
|
|
gptkbp:developer
|
5 years
|
|
gptkbp:diameter
|
3.9 meters
|
|
gptkbp:emergency_services
|
abort system
|
|
gptkbp:features
|
conical shape
|
|
gptkbp:first_flight
|
gptkb:Apollo_17
gptkb:Apollo_1
|
|
gptkbp:historical_event
|
first crewed lunar landing
|
|
gptkbp:historical_significance
|
moon landing missions
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
The command module
|
|
gptkbp:influenced_by
|
previous spacecraft
|
|
gptkbp:inspiration
|
gptkb:Author
|
|
gptkbp:instrument
|
navigation and control
|
|
gptkbp:is_involved_in
|
Lunar Module operations
|
|
gptkbp:is_tested_for
|
simulator tests
|
|
gptkbp:landing_site
|
gptkb:Pacific_Ocean
|
|
gptkbp:launch_date
|
1966-02-21
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
|
|
gptkbp:legacy
|
gptkb:spacecraft
|
|
gptkbp:length
|
3.9 meters
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:max_takeoff_weight
|
splashdown
|
|
gptkbp:mission
|
gptkb:Apollo_17
gptkb:Apollo_8
|
|
gptkbp:mission_duration
|
up to 12 days
|
|
gptkbp:navigation_system
|
star tracker
|
|
gptkbp:operational_area
|
command and control
1967-1972
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:part_of
|
gptkb:software
|
|
gptkbp:power_output
|
fuel cells
|
|
gptkbp:primary_function
|
crew transport
|
|
gptkbp:related_model
|
gptkb:Apollo_CSM
|
|
gptkbp:restoration
|
gptkb:USS_Hornet
|
|
gptkbp:safety_features
|
gptkb:musician
|
|
gptkbp:scholarships
|
oxygen and water
|
|
gptkbp:seating_capacity
|
limited
|
|
gptkbp:services
|
attached
|
|
gptkbp:speed
|
capable
25,000 mph
|
|
gptkbp:successor
|
gptkb:Orion_spacecraft
|
|
gptkbp:surface
|
reaction control thrusters
|
|
gptkbp:used_in
|
gptkb:Apollo_missions
|
|
gptkbp:weight
|
5,000 pounds
|
|
gptkbp:bfsParent
|
gptkb:Apollo_11_mission_insignia
|
|
gptkbp:bfsLayer
|
4
|