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gptkbp:instance_of
|
gptkb:software
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Apollo_Command_Module_Yankee_Clipper
gptkb:Apollo_Command_Module_Endeavour
|
|
gptkbp:communication
|
S-band radio
|
|
gptkbp:controls
|
Inertial navigation system
|
|
gptkbp:cooling_system
|
gptkb:Phenolic-impregnated_carbon_ablator
|
|
gptkbp:crew
|
gptkb:David_Scott
gptkb:3
gptkb:Alfred_Worden
gptkb:James_Irwin
gptkb:engine
|
|
gptkbp:design
|
Lunar missions
|
|
gptkbp:designed_by
|
gptkb:North_American_Aviation
|
|
gptkbp:diameter
|
3.9 m
|
|
gptkbp:elevation
|
200 km
|
|
gptkbp:first_flight
|
gptkb:Apollo_17
gptkb:Apollo_7
gptkb:Apollo_9
|
|
gptkbp:game_world
|
August 7, 1971
|
|
gptkbp:historical_significance
|
Key component of lunar exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Apollo Command Module America
|
|
gptkbp:influenced
|
Future spacecraft design
|
|
gptkbp:influenced_by
|
Mercury and Gemini programs
|
|
gptkbp:inspiration
|
Future space missions
|
|
gptkbp:involved_units
|
gptkb:15
|
|
gptkbp:landing_site
|
August 7, 1971
|
|
gptkbp:launch_date
|
July 26, 1971
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
|
|
gptkbp:launched
|
July 26, 1971
|
|
gptkbp:legacy
|
Pioneering human spaceflight.
|
|
gptkbp:length
|
3.2 m
|
|
gptkbp:manufacturer
|
gptkb:Rockwell_International
|
|
gptkbp:max_takeoff_weight
|
Splashdown
|
|
gptkbp:mission
|
gptkb:Apollo_15
Successful
Manned lunar exploration
Museum display
|
|
gptkbp:mission_duration
|
12 days, 7 hours, 12 minutes
|
|
gptkbp:notable_feature
|
Three-module design
|
|
gptkbp:operational_area
|
1967-1972
|
|
gptkbp:operational_status
|
Retired
|
|
gptkbp:part_of
|
gptkb:software
|
|
gptkbp:power_output
|
Fuel cells
|
|
gptkbp:primary_function
|
Crew transport and command
|
|
gptkbp:research
|
Lunar surface exploration
|
|
gptkbp:restoration
|
gptkb:USS_Okinawa
|
|
gptkbp:safety_features
|
Parachute recovery system
|
|
gptkbp:significant_event
|
First crewed mission to land on the Moon
|
|
gptkbp:speed
|
39,000 km/h
|
|
gptkbp:successor
|
gptkb:Orion_spacecraft
|
|
gptkbp:weight
|
5,900 kg
|