|
gptkbp:instanceOf
|
launch vehicle
|
|
gptkbp:affiliatedWith
|
Korea_Space_Program
|
|
gptkbp:country
|
gptkb:South_Korea
|
|
gptkbp:developedBy
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:engineConfiguration
|
staged combustion cycle
|
|
gptkbp:engineType
|
liquid-fueled
|
|
gptkbp:firstPublished
|
2013
|
|
gptkbp:fuelType
|
RP-1 and liquid oxygen
|
|
gptkbp:futurePlans
|
gptkb:KSLV-III
|
|
gptkbp:historicalSignificance
|
first South Korean launch vehicle
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Korea Space Launch Vehicle family
|
|
gptkbp:internationalCooperation
|
gptkb:Russia
|
|
gptkbp:launchDate
|
KSLV-1_and_KSLV-2
|
|
gptkbp:launched
|
gptkb:Korea_Aerospace_Research_Institute
annual
ground control
varies by mission
estimated $20 million
|
|
gptkbp:launchSite
|
gptkb:Naro_Space_Center
|
|
gptkbp:launchVehicle
|
gptkb:KSLV-2
gptkb:KSLV-1
gptkb:KSLV
2
modular design
two-stage
expendable launch vehicle
|
|
gptkbp:majorRivers
|
5
|
|
gptkbp:manufacturer
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:missileSystem
|
first stage
second stage
|
|
gptkbp:missions
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:notableFeature
|
2010
KoreaSat-5A
|
|
gptkbp:numberOfStudents
|
2
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:orbitalInclination
|
3
varies by mission
|
|
gptkbp:passenger_traffic
|
geostationary transfer orbit
diameter 3.0 m
low_Earth_orbit
|
|
gptkbp:payloadCapacity
|
1000 kg to Low Earth Orbit
|
|
gptkbp:productionCompany
|
retired
|
|
gptkbp:propulsion
|
300 kN
|
|
gptkbp:provides
|
inertial navigation system
|
|
gptkbp:purpose
|
satellite launch
|
|
gptkbp:reliability
|
none
|
|
gptkbp:researchAndDevelopment
|
ongoing
|
|
gptkbp:safetyFeatures
|
mixed
|
|
gptkbp:successor
|
gptkb:KSLV-II
|
|
gptkbp:technology
|
international partners
|