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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:bfsLayer
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4
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gptkbp:bfsParent
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gptkb:Gemini_3
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gptkbp:artwork
|
off the coast of Florida
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|
gptkbp:communication
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S-band radio
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gptkbp:controls
|
manual and automatic controls
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|
gptkbp:cooling_system
|
phenolic resin
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gptkbp:crew
|
gptkb:John_Young
gptkb:Gus_Grissom
2
extensive training program
continuous monitoring during flight
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|
gptkbp:debut_year
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gptkb:Gemini_3
|
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gptkbp:decommissioned
|
gptkb:1966
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gptkbp:diameter
|
3.1 m
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|
gptkbp:first_flight
|
gptkb:Gemini_3
gptkb:Gemini_1
|
|
gptkbp:historical_significance
|
pioneered spaceflight technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Gemin 3 Command Module
|
|
gptkbp:influenced
|
subsequent spacecraft designs
|
|
gptkbp:inspiration
|
future Apollo missions
|
|
gptkbp:landing_site
|
gptkb:Atlantic_Ocean
|
|
gptkbp:launch_date
|
March 23, 1966
11:00 AMEST
|
|
gptkbp:launch_site
|
gptkb:Cape_Kennedy_Air_Force_Station
|
|
gptkbp:launch_vehicle
|
Titan IIGLV
|
|
gptkbp:launched
|
March 23, 1966
|
|
gptkbp:legacy
|
important step in human space exploration
|
|
gptkbp:length
|
3.9 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Aircraft_Corporation
|
|
gptkbp:mission
|
gptkb:spacecraft
gptkb:Gemini_12
gptkb:3
gptkb:Houston,_Texas
gptkb:NASA_Mission_Control_Center
successful
detailed analysis conducted
first American spacecraft to carry a crew in orbit
|
|
gptkbp:mission_duration
|
8 days
|
|
gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:objective
|
demonstrate orbital flight capabilities
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_inclination
|
28.5 degrees
|
|
gptkbp:part_of
|
gptkb:Gemini_program
|
|
gptkbp:power_output
|
solar panels
|
|
gptkbp:safety_features
|
multiple redundancy systems
|
|
gptkbp:scholarships
|
environmental control system
|
|
gptkbp:speed
|
28,000 km/h
6 degrees
|
|
gptkbp:successor
|
gptkb:Gemini_4_Command_Module
|
|
gptkbp:team
|
gptkb:USS_Intrepid
|
|
gptkbp:weight
|
3,000 kg
|