Atlas Agena

GPTKB entity

Statements (59)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:configuration two-stage rocket
gptkbp:debut over 100 launches
gptkbp:development_cost estimated at $100 million
gptkbp:diameter 3.05 meters
gptkbp:engine_type gptkb:Team_Rocket
gptkbp:first_flight 1959-12-29
1987-12-12
gptkbp:flight_style over 100
gptkbp:fuel_type RP-1 and liquid oxygen
gptkbp:guidance_system inertial guidance system
gptkbp:has_tour expendable launch system
gptkbp:height 23.5 meters
https://www.w3.org/2000/01/rdf-schema#label Atlas Agena
gptkbp:launch_mass approximately 20,000 kg
gptkbp:launch_site gptkb:Cape_Canaveral_Space_Force_Station
gptkbp:launch_vehicle gptkb:Atlas
gptkbp:manufacturer gptkb:Lockheed_Martin
gptkbp:notable_launches first spacecraft to fly by Saturn
first spacecraft to orbit Mars
first spacecraft to fly by Jupiter
first spacecraft to fly by Pluto
first spacecraft to land on Mars
first spacecraft to fly by Neptune
first spacecraft to fly by Uranus
first spacecraft to fly by the Laniakea Supercluster
first spacecraft to fly by the Andromeda Galaxy
first spacecraft to fly by the Centaurus Cluster
first spacecraft to fly by the Coma Cluster
first spacecraft to fly by the Fornax Cluster
first spacecraft to fly by the Great Attractor
first spacecraft to fly by the Hercules Cluster
first spacecraft to fly by the Kuiper Belt
first spacecraft to fly by the Milky Way Galaxy
first spacecraft to fly by the Oort Cloud
first spacecraft to fly by the Perseus Cluster
first spacecraft to fly by the Sculptor Group
first spacecraft to fly by the Virgo Cluster
first spacecraft to fly by the heliopause
first spacecraft to fly by the interstellar medium
first successful launch of a spacecraft to Venus
first spacecraft to fly by the Local Group of Galaxies
first spacecraft to fly by the Pisces-Perseus Supercluster
first spacecraft to fly by the Cosmic Microwave Background.
gptkbp:notable_mission gptkb:Lunar_Orbiter_1
gptkb:Viking_1
gptkb:Gemini_missions
gptkb:Mariner_2
gptkb:Pioneer_10
gptkbp:operational_period 1959 to 1987
gptkbp:operational_use military and civilian missions
gptkbp:payload_capacity up to 1,500 kg to low Earth orbit
4.6 meters in diameter
gptkbp:predecessor gptkb:Atlas_D
gptkbp:success_rate approximately 90%
gptkbp:successor gptkb:Atlas_V
gptkbp:used_for gptkb:Space_Launch_System
gptkbp:bfsParent gptkb:Space_Launch_Complex_19
gptkbp:bfsLayer 5