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gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:communication_system
|
S-band radio
|
|
gptkbp:control_system
|
gptkb:navigation_system
|
|
gptkbp:crew
|
gptkb:NASA_Astronaut_Training_Program
gptkb:N/_A
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:design_features
|
gptkb:health_services
gptkb:safety_equipment
gptkb:Command_Line_Interface
gptkb:Team_Rocket
gptkb:Public_service
gptkb:shield
modular design
advanced avionics
reusable components
crew cabin
|
|
gptkbp:first_flight
|
gptkb:N/_A
|
|
gptkbp:height
|
3.2 m
|
|
gptkbp:historical_significance
|
part of the Apollo program's legacy
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Apollo 62 spacecraft
|
|
gptkbp:inspiration
|
future lunar missions
|
|
gptkbp:landing_site
|
gptkb:N/_A
|
|
gptkbp:launch_date
|
1972-04-16
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:mission
|
gptkb:Houston,_Texas
gptkb:Moon
Apollo 62 mission patch
|
|
gptkbp:mission_duration
|
14 days
|
|
gptkbp:mission_type
|
gptkb:Mars_Rover
|
|
gptkbp:orbital_altitude
|
7.8 km/s
|
|
gptkbp:part_of
|
gptkb:Apollo_program
|
|
gptkbp:power_source
|
fuel cells
|
|
gptkbp:related_to
|
gptkb:Apollo_14
gptkb:Apollo_16
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_11
gptkb:Apollo_13
gptkb:Apollo_12
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
redundant systems
thermal protection system
|
|
gptkbp:scientific_instruments
|
gptkb:Lunar_Module
gptkb:camera
gptkb:spectrometer
gptkb:magnetometer
sample return system
|
|
gptkbp:status
|
cancelled
|
|
gptkbp:successor
|
gptkb:Apollo_17
|
|
gptkbp:weight
|
45,000 kg
|
|
gptkbp:width
|
4.2 m
|
|
gptkbp:bfsParent
|
gptkb:James_Arthur_Lovell_Jr.
|
|
gptkbp:bfsLayer
|
6
|