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
|