Statements (57)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
launch vehicle
|
| gptkbp:built |
overcame various engineering challenges
|
| gptkbp:collaborations |
with various space agencies
formed international partnerships for missions |
| gptkbp:community_engagement |
high levels of public engagement during launches
high public interest in launches |
| gptkbp:community_outreach |
educational outreach programs initiated
|
| gptkbp:compatibleWith |
compatible with various satellites
|
| gptkbp:construction_cost |
approximately $1 billion
|
| gptkbp:controls |
digital flight control system
|
| gptkbp:country |
gptkb:South_Korea
|
| gptkbp:design |
10 years
|
| gptkbp:diameter |
3.5 meters
|
| gptkbp:engineType |
liquid rocket engine
|
| gptkbp:environmental_impact |
assessed for environmental impact
|
| gptkbp:firstFlight |
2020-10-21
multiple test flights conducted |
| gptkbp:fuelType |
RP-1 and liquid oxygen
|
| gptkbp:future_plans |
2006 to 2020
|
| gptkbp:futurePlans |
planned future upgrades to enhance capabilities
|
| gptkbp:height |
47.2 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
KSLV-2
|
| gptkbp:launchDate |
1-2 times per year
conducted after each launch multiple launches since 2020 |
| gptkbp:launched |
2022-06-21
ground control operations specific launch windows required |
| gptkbp:launchSite |
gptkb:Korea_Aerospace_Research_Institute
gptkb:Naro_Space_Center |
| gptkbp:launchVehicle |
gptkb:KSLV
two-stage rocket compared with other launch vehicles modern design principles applied |
| gptkbp:manufacturer |
gptkb:Korea_Aerospace_Research_Institute
|
| gptkbp:media_coverage |
extensive media coverage during launches
|
| gptkbp:mission |
aligned with national space exploration goals
|
| gptkbp:missions |
gptkb:Korea_Aerospace_Research_Institute
planned for various scientific missions Korea's_first_lunar_orbiter_mission |
| gptkbp:number_of_stages |
2
|
| gptkbp:operational_status |
active
|
| gptkbp:orbitalInclination |
achieved during missions
|
| gptkbp:passenger_traffic |
4 meters in diameter
modular payload integration 1.5 tons to geostationary transfer orbit |
| gptkbp:performances |
detailed technical specifications available
|
| gptkbp:propulsion |
300 kN
|
| gptkbp:provides |
inertial navigation system
technical support from various organizations |
| gptkbp:purpose |
satellite launch
|
| gptkbp:reliability |
high reliability expected
|
| gptkbp:research |
supports scientific research missions.
|
| gptkbp:researchAndDevelopment |
ongoing research and development efforts
|
| gptkbp:revenue |
high commercial potential for satellite launches
|
| gptkbp:safetyFeatures |
strict safety measures in place
|
| gptkbp:successor |
gptkb:KSLV-3
|