|
gptkbp:instance_of
|
gptkb:Command_Line_Interface
|
|
gptkbp:associated_with
|
gptkb:Moon
gptkb:NASA's_Apollo_program
gptkb:human_spaceflight
space exploration history
spacecraft technology
|
|
gptkbp:crew
|
gptkb:John_Young
gptkb:Vance_Brand
gptkb:Thomas_Stafford
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:decommissioned
|
gptkb:1975
|
|
gptkbp:design_features
|
gptkb:parachute
ablative heat shield
command module docking system
|
|
gptkbp:designed_by
|
gptkb:North_American_Aviation
|
|
gptkbp:diameter
|
12 feet 10 inches
|
|
gptkbp:first_flight
|
gptkb:Apollo_20
gptkb:Apollo_1
|
|
gptkbp:flight_style
|
gptkb:1
|
|
gptkbp:historical_significance
|
part of lunar exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Command Module 20
|
|
gptkbp:inspiration
|
gptkb:future_space_missions
|
|
gptkbp:instruments
|
gptkb:communication_systems
navigation systems
life support systems
|
|
gptkbp:landing_site
|
gptkb:Pacific_Ocean
|
|
gptkbp:launch_date
|
April 1972
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
|
|
gptkbp:launched
|
gptkb:NASA
|
|
gptkbp:legacy
|
influenced future spacecraft design
|
|
gptkbp:length
|
11 feet 3 inches
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:mission
|
successful
lunar orbit
|
|
gptkbp:mission_duration
|
10 days
|
|
gptkbp:notable_event
|
crew recovery
lunar orbit insertion
scientific experiments conducted
Apollo 20 mission
reentry and splashdown
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:part_of
|
gptkb:Apollo_program
|
|
gptkbp:primary_function
|
command and control
crew transport
|
|
gptkbp:recovery_method
|
April 1972
|
|
gptkbp:speed
|
25,000 mph
|
|
gptkbp:successor
|
gptkb:Orion_spacecraft
|
|
gptkbp:team
|
gptkb:USS_Hornet
|
|
gptkbp:used_in
|
Apollo 20 mission
|
|
gptkbp:weight
|
5,000 pounds
|
|
gptkbp:bfsParent
|
gptkb:Apollo_20_spacecraft
|
|
gptkbp:bfsLayer
|
7
|