|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:control_system
|
gptkb:navigation_system
|
|
gptkbp:development
|
2002-2009
|
|
gptkbp:diameter
|
3.0 meters
|
|
gptkbp:engine_configuration
|
four clustered engines
|
|
gptkbp:engine_type
|
KRE-75
|
|
gptkbp:first_flight
|
multiple
October 2009
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:guidance_system
|
autonomous guidance
|
|
gptkbp:height
|
25.8 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
KSLV-1 first stage
|
|
gptkbp:launch_site
|
gptkb:Naro_Space_Center
|
|
gptkbp:launch_vehicle
|
KSLV
|
|
gptkbp:manufacturer
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:mass
|
130,000 kg
|
|
gptkbp:mission
|
gptkb:Space_Launch_System
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:propulsion
|
RP-1 and Liquid Oxygen
3000 k N
|
|
gptkbp:role
|
provides initial thrust
|
|
gptkbp:stage_separation
|
after 150 seconds
|
|
gptkbp:success_rate
|
50%
|
|
gptkbp:used_in
|
KSLV-1 launch vehicle
|
|
gptkbp:bfsParent
|
gptkb:KSLV-1_second_stage
|
|
gptkbp:bfsLayer
|
7
|