|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:control_system
|
Digital control system
|
|
gptkbp:country
|
gptkb:South_Korea
|
|
gptkbp:debut
|
2 launches total.
|
|
gptkbp:design
|
gptkb:N/_A
|
|
gptkbp:development
|
gptkb:2002
|
|
gptkbp:development_cost
|
$400 million
|
|
gptkbp:diameter
|
3.0 meters
|
|
gptkbp:engine_type
|
Liquid-fueled
|
|
gptkbp:first_flight
|
2009-08-25
|
|
gptkbp:fuel_type
|
gptkb:liquid
|
|
gptkbp:guidance_system
|
Inertial navigation system
|
|
gptkbp:height
|
33 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
KSLV-1 rocket
|
|
gptkbp:launch_date
|
gptkb:N/_A
2009-08-25
|
|
gptkbp:launch_event
|
gptkb:Mixed
50%
|
|
gptkbp:launch_mass
|
140 tons
|
|
gptkbp:launch_platform
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:launch_site
|
gptkb:Naro_Space_Center
|
|
gptkbp:launch_vehicle
|
Expendable launch vehicle
KSLV
Single configuration.
|
|
gptkbp:launch_window
|
gptkb:N/_A
|
|
gptkbp:launched
|
2
|
|
gptkbp:manufacturer
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:mission_type
|
Scientific
|
|
gptkbp:notable_launches
|
gptkb:STSAT-2
|
|
gptkbp:number_of_engines
|
gptkb:3
|
|
gptkbp:number_of_stages
|
gptkb:3
gptkb:KSLV-1
KRE-75
|
|
gptkbp:operational_period
|
2009-2013
|
|
gptkbp:operational_status
|
Retired
|
|
gptkbp:orbital_launches
|
2
|
|
gptkbp:payload_capacity
|
Low Earth Orbit
1000 kg to Low Earth Orbit
2.5 meters diameter
|
|
gptkbp:propulsion
|
3000 k N
|
|
gptkbp:purpose
|
Satellite launch
|
|
gptkbp:replaced_by
|
gptkb:KSLV-2
|
|
gptkbp:strategic_goals
|
gptkb:1
|
|
gptkbp:success
|
gptkb:1
|
|
gptkbp:bfsParent
|
gptkb:KSLV-1_second_stage
|
|
gptkbp:bfsLayer
|
7
|