|
gptkbp:instanceOf
|
launch vehicle
|
|
gptkbp:collaborations
|
yes
|
|
gptkbp:controls
|
inertial navigation system
|
|
gptkbp:country
|
gptkb:South_Korea
|
|
gptkbp:design
|
Korean
|
|
gptkbp:diameter
|
2.9 meters
|
|
gptkbp:educational_programs
|
Korean_space_program
|
|
gptkbp:engineConfiguration
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:engineType
|
liquid fuel
|
|
gptkbp:firstFlight
|
2009
|
|
gptkbp:height
|
33 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
KSLV
|
|
gptkbp:launchDate
|
low
multiple launches
|
|
gptkbp:launched
|
2013
4
|
|
gptkbp:launchSite
|
gptkb:Naro_Space_Center
|
|
gptkbp:launchVehicle
|
gptkb:KSLV_family
expendable launch vehicle
|
|
gptkbp:manufacturer
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:missions
|
gptkb:Naro-1
|
|
gptkbp:number_of_stages
|
gptkb:KSLV-1
2
|
|
gptkbp:offers
|
estimated 50 million USD
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbitalInclination
|
yes
|
|
gptkbp:passenger_traffic
|
3.0 meters
1000 kg to LEO
|
|
gptkbp:productionYears
|
2002-2013
|
|
gptkbp:provides
|
autonomous guidance system
|
|
gptkbp:purpose
|
satellite launch
|
|
gptkbp:reliability
|
moderate
|
|
gptkbp:succeededBy
|
50%
|
|
gptkbp:successor
|
gptkb:KSLV-II
|
|
gptkbp:weight
|
140 tons
|