|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
manual and automatic
|
|
gptkbp:aircraft_operated
|
12 missions
|
|
gptkbp:associated_with
|
gptkb:Gemini_missions
|
|
gptkbp:communication_system
|
S-band
|
|
gptkbp:control_system
|
reaction control system
|
|
gptkbp:data_transmission
|
telemetry
|
|
gptkbp:decommissioned
|
gptkb:1966
|
|
gptkbp:design
|
14 days
|
|
gptkbp:designed_for
|
gptkb:Gemini_program
|
|
gptkbp:development
|
1962-1965
|
|
gptkbp:diameter
|
3.05 m
|
|
gptkbp:financial_stability
|
gyroscopic stabilization
|
|
gptkbp:first_flight
|
yes
1965-03-16
1966-11-11
|
|
gptkbp:guidance_system
|
inertial guidance
|
|
gptkbp:has_units
|
gptkb:12
|
|
gptkbp:height
|
3.05 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Gemini Agena Target Vehicle
|
|
gptkbp:launch_date
|
1965-03-16
1966-11-11
|
|
gptkbp:launch_mass
|
1,500 kg
|
|
gptkbp:launch_site
|
gptkb:Cape_Kennedy_Air_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Titan_II_GLV
|
|
gptkbp:launched
|
gptkb:12
gptkb:NASA
|
|
gptkbp:length
|
4.88 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Aircraft_Corporation
|
|
gptkbp:mass
|
1,500 kg
|
|
gptkbp:mission
|
gptkb:Gemini_12
gptkb:Gemini_8
gptkb:Gemini_10
gptkb:Gemini_11
|
|
gptkbp:mission_duration
|
up to 14 days
|
|
gptkbp:mission_type
|
target vehicle
|
|
gptkbp:operated_by
|
gptkb:NASA
|
|
gptkbp:operational_period
|
1965-1966
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
space rendezvous
|
|
gptkbp:orbit_type
|
low Earth orbit
|
|
gptkbp:payload_capacity
|
1,000 kg
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:primary_function
|
docking target
|
|
gptkbp:propulsion
|
liquid rocket
|
|
gptkbp:significance
|
first spacecraft to be used as a target for manned missions.
|
|
gptkbp:speed
|
no
|
|
gptkbp:successor
|
gptkb:Agena_D
|
|
gptkbp:used_for
|
docking practice
|
|
gptkbp:bfsParent
|
gptkb:James_Arthur_Lovell_Jr.
|
|
gptkbp:bfsLayer
|
6
|