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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
|
gptkb:Gemini_12
gptkb:Gemini_8
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gptkbp:communication
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gptkb:aircraft
|
|
gptkbp:controls
|
autonomous control system
|
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gptkbp:country
|
none known
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gptkbp:decommissioned
|
gptkb:1980
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gptkbp:design
|
modified version of the Agena spacecraft
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gptkbp:developer
|
1956 to 1959
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gptkbp:diameter
|
approximately 1.5 m
|
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gptkbp:elevation
|
low Earth orbit
|
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gptkbp:features
|
modular design
|
|
gptkbp:first_flight
|
gptkb:1959
gptkb:1980
over 100
|
|
gptkbp:guidance_system
|
inertial guidance system
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|
gptkbp:has_programs
|
Gemini, Apollo
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|
gptkbp:historical_significance
|
pioneered rendezvous techniques
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Agena Target Vehicle
|
|
gptkbp:is_used_by
|
gptkb:NASA
|
|
gptkbp:launch_date
|
varied by mission
1959 to 1980
|
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gptkbp:launch_site
|
gptkb:cape
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas_rocket
approximately 1,500 kg
expendable launch vehicle
|
|
gptkbp:launched
|
over 100 launches
|
|
gptkbp:legacy
|
influenced future spacecraft designs
|
|
gptkbp:length
|
approximately 3.5 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:mission
|
gptkb:1980
gptkb:Gemini_program
scientific and military missions
|
|
gptkbp:notable_users
|
NASA, USAF
|
|
gptkbp:operated_by
|
gptkb:aircraft
|
|
gptkbp:operational_area
|
21 years
space environment
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:power_output
|
solar panels
|
|
gptkbp:primary_function
|
target for rendezvous missions
|
|
gptkbp:propulsion
|
gptkb:rocket
|
|
gptkbp:provides_information_on
|
telemetry data link
|
|
gptkbp:purpose
|
target vehicle for spacecraft
test vehicle for missile systems
|
|
gptkbp:seating_capacity
|
up to 1,000 kg
|
|
gptkbp:speed
|
gptkb:battle
|
|
gptkbp:succeeded_by
|
approximately 90%
|
|
gptkbp:successor
|
gptkb:Agena_D
|
|
gptkbp:used_in
|
military applications
|
|
gptkbp:variant
|
multiple variants
|
|
gptkbp:weight
|
approximately 1,500 kg
|