|
gptkbp:instanceOf
|
launch vehicle
|
|
gptkbp:affiliatedWith
|
Korean_Space_Program
|
|
gptkbp:country
|
gptkb:South_Korea
|
|
gptkbp:designedBy
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:developer
|
approximately $400 million
2002 to 2013
|
|
gptkbp:diameter
|
3.0 meters
|
|
gptkbp:education
|
increased interest in aerospace engineering
|
|
gptkbp:engineConfiguration
|
single core with strap-on boosters
|
|
gptkbp:engineType
|
liquid-fueled
|
|
gptkbp:firstFlight
|
2010
conducted before operational launches
|
|
gptkbp:firstPublished
|
2013
|
|
gptkbp:futurePlans
|
development_of_KSLV-III
|
|
gptkbp:height
|
33 meters
|
|
gptkbp:homeGround
|
used for pre-launch operations
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Korea Space Launch Vehicle
|
|
gptkbp:internationalClassification
|
part of global space community
|
|
gptkbp:internationalCooperation
|
with_Russia
|
|
gptkbp:launchDate
|
multiple launches
|
|
gptkbp:launched
|
annual
varies by mission
approximately $30 million per launch
located_at_Naro_Space_Center
|
|
gptkbp:launchSite
|
gptkb:Naro_Space_Center
5
140 tons
|
|
gptkbp:launchVehicle
|
gptkb:KSLV_family
2
expendable launch vehicle
|
|
gptkbp:legacy
|
foundation_for_future_Korean_space_endeavors
|
|
gptkbp:manufacturer
|
gptkb:Korea_Aerospace_Industries
|
|
gptkbp:marketSegment
|
satellite communications
|
|
gptkbp:missions
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:notableFeature
|
STSAT-2B
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:orbitalInclination
|
90 degrees
|
|
gptkbp:passenger_traffic
|
4 meters in diameter
in_Low_Earth_Orbit
|
|
gptkbp:payloadCapacity
|
1,500 kg to Low Earth Orbit
|
|
gptkbp:propulsion
|
300 kN
|
|
gptkbp:provides
|
inertial navigation
|
|
gptkbp:purpose
|
satellite launch
|
|
gptkbp:reliability
|
moderate
|
|
gptkbp:researchInterest
|
scientific satellites
|
|
gptkbp:successor
|
gptkb:KSLV-II
|