|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:communication_system
|
gptkb:radio_station
S-band radio
UHF radio
|
|
gptkbp:control_system
|
gptkb:navigation_system
reaction control thrusters
|
|
gptkbp:debut
|
gptkb:1959
gptkb:1980
gptkb:1987
|
|
gptkbp:decommissioned
|
gptkb:1980
gptkb:1987
|
|
gptkbp:design
|
gptkb:Agena_series
|
|
gptkbp:design_purpose
|
target vehicle for testing
|
|
gptkbp:designed_by
|
gptkb:Lockheed_Martin
|
|
gptkbp:designed_for
|
gptkb:space_mission
docking maneuvers
|
|
gptkbp:developed_by
|
gptkb:Lockheed_Martin
|
|
gptkbp:development
|
1956-1959
|
|
gptkbp:diameter
|
2.4 m
1.5 meters
2.4 meters
approximately 2.4 m
|
|
gptkbp:features
|
modular design
high maneuverability
advanced telemetry systems
reconfigurable payloads
multiple mission profiles
|
|
gptkbp:first_flight
|
gptkb:1959
gptkb:1962
gptkb:1980
|
|
gptkbp:flight_style
|
over 100
|
|
gptkbp:guidance_system
|
inertial navigation
star tracker
|
|
gptkbp:has_ability
|
gptkb:scientific_experiments
satellite deployment
orbital rendezvous
|
|
gptkbp:has_units
|
over 100
over 20
|
|
gptkbp:height
|
3.6 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Agena target vehicle
|
|
gptkbp:influenced_by
|
gptkb:Orion_spacecraft
gptkb:spacecraft
gptkb:International_Space_Station
gptkb:Space_Shuttle
|
|
gptkbp:involved_in
|
military applications
scientific research missions
space technology demonstrations
Apollo program training
satellite reconnaissance missions
|
|
gptkbp:launch_date
|
gptkb:1966
|
|
gptkbp:launch_mass
|
1,500 kg
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas_rocket
|
|
gptkbp:launched
|
over 100
over 100 missions
|
|
gptkbp:legacy
|
influenced future spacecraft designs
|
|
gptkbp:length
|
3.6 m
3.6 meters
approximately 4.5 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:mass
|
1,500 kg
|
|
gptkbp:mission
|
gptkb:Gemini_12
gptkb:Gemini_8
|
|
gptkbp:mission_type
|
military and civilian
target vehicle
|
|
gptkbp:notable_features
|
modular design
high maneuverability
reusable components
advanced telemetry system
|
|
gptkbp:notable_mission
|
gptkb:Pioneer_11
gptkb:Apollo_14
gptkb:Mariner_5
gptkb:Apollo_10
gptkb:Apollo_16
gptkb:Mars_Pathfinder
gptkb:Mars_Rover
gptkb:New_Horizons
gptkb:OSIRIS-REx
gptkb:Lunar_Orbiter_1
gptkb:Viking_1
gptkb:Gemini_12
gptkb:Lunar_Orbiter_2
gptkb:Lunar_Orbiter_3
gptkb:Lunar_Orbiter_4
gptkb:Mars_Reconnaissance_Orbiter
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Mars_Science_Laboratory
gptkb:Apollo_9
gptkb:Apollo_11
gptkb:Juno
gptkb:Apollo_13
gptkb:Parker_Solar_Probe
gptkb:Mariner_6
gptkb:Apollo_12
gptkb:Dawn
gptkb:Gemini_8
gptkb:Voyager_1
gptkb:Voyager_2
gptkb:Mariner_7
gptkb:Gemini_10
gptkb:Pioneer_10
gptkb:Viking_2
gptkb:Kepler
gptkb:Lunar_Orbiter_5
gptkb:Gemini_11
Gemini 8 docking
|
|
gptkbp:operated_by
|
gptkb:US_Air_Force
gptkb:United_States_Air_Force
gptkb:National_Reconnaissance_Office
gptkb:NASA
|
|
gptkbp:operational_period
|
21 years
1962-1980
1959-1980
1959-1987
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbit_type
|
low Earth orbit
|
|
gptkbp:orbital_altitude
|
approximately 300 km
200 km to 1,000 km
|
|
gptkbp:orbital_inclination
|
varied
|
|
gptkbp:payload_capacity
|
up to 1,000 kg
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:primary_function
|
satellite deployment
|
|
gptkbp:primary_mission
|
target for manned missions
|
|
gptkbp:propulsion
|
gptkb:Team_Rocket
|
|
gptkbp:purpose
|
target vehicle for docking
|
|
gptkbp:reliability
|
high
|
|
gptkbp:replaced_by
|
gptkb:Advanced_Targeting_System
|
|
gptkbp:significant_event
|
first successful docking with Gemini 8
|
|
gptkbp:successor
|
gptkb:Centaur
gptkb:Centaur_program
gptkb:Agena_D
gptkb:Gemini_spacecraft
|
|
gptkbp:system
|
gptkb:Mars_program
gptkb:Lunar_Orbiter_program
gptkb:Viking_program
gptkb:Apollo_program
gptkb:Voyager_program
gptkb:Gemini_program
gptkb:Pioneer_program
gptkb:Mariner_program
gptkb:Earth_observation
Space science missions
Astrophysics missions
Planetary exploration missions
Surveyor program
Space technology demonstrations
International cooperation missions
Space research missions
Launch vehicle testing missions
Orbital mechanics studies
Satellite reconnaissance missions
Spacecraft docking technology development
Spacecraft rendezvous missions
|
|
gptkbp:used_by
|
gptkb:US_Air_Force
gptkb:NASA
|
|
gptkbp:used_for
|
gptkb:scientific_experiments
satellite deployment
|
|
gptkbp:used_in
|
gptkb:Apollo_program
gptkb:Gemini_program
gptkb:NASA_missions
|
|
gptkbp:weight
|
1,500 kg
approximately 1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Gemini_12
gptkb:Gemini_8
gptkb:NASA's_Gemini_program
|
|
gptkbp:bfsLayer
|
5
|