|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:check_in_time
|
300 seconds
|
|
gptkbp:configuration
|
gptkb:Agena_D
|
|
gptkbp:control_system
|
reaction control system
|
|
gptkbp:development
|
1950s
|
|
gptkbp:diameter
|
3.05 meters
|
|
gptkbp:engine_type
|
gptkb:Rocketdyne_LR89
|
|
gptkbp:first_flight
|
1960-12-18
1978-05-30
|
|
gptkbp:guidance_system
|
inertial guidance
|
|
gptkbp:height
|
23.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Atlas LV-3 Agena D
|
|
gptkbp:launch_mass
|
12,000 kg
|
|
gptkbp:launch_site
|
gptkb:Vandenberg_Space_Force_Base
gptkb:Cape_Canaveral_Air_Force_Station
|
|
gptkbp:launch_vehicle
|
Atlas family
|
|
gptkbp:launched
|
80
Complex 14
Complex 3
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:mass
|
12,000 kg
|
|
gptkbp:mission_type
|
gptkb:space_mission
gptkb:missions
|
|
gptkbp:notable_achievements
|
first spacecraft to Venus
first lunar orbiter
first spacecraft to Mars
|
|
gptkbp:notable_launches
|
gptkb:Lunar_Orbiter_1
gptkb:Viking_1
gptkb:Gemini_missions
gptkb:Mariner_2
|
|
gptkbp:number_of_stages
|
gptkb:Atlas_D
gptkb:Agena_D
2
|
|
gptkbp:operational_period
|
1960-1978
|
|
gptkbp:payload_capacity
|
4.2 meters
1,500 kg to Low Earth Orbit
|
|
gptkbp:predecessor
|
gptkb:Atlas_LV-3_Agena_B
|
|
gptkbp:primary_function
|
orbital insertion
spacecraft support
|
|
gptkbp:propulsion
|
150 k N
|
|
gptkbp:retired
|
gptkb:1978
|
|
gptkbp:success_rate
|
90%+
|
|
gptkbp:successor
|
gptkb:Atlas_V
|
|
gptkbp:used_for
|
satellite launches
|
|
gptkbp:bfsParent
|
gptkb:Mariner_4
|
|
gptkbp:bfsLayer
|
4
|