Next-Generation Launch Vehicle(KSLV-III)
- Development Period : 2023.07 ⁓ 2032.12
- Development Budget : KRW 2,013.2 billion
In July 2023, KARI initiated the Next-Generation Launch Vehicle Development Project to address national space development demands, such as satellite launches and space exploration and secure autonomous exploration capabilities. The project aims to develop a next-generation launch vehicle for large satellite deployment and space exploration, with three launches scheduled by 2032. To this end, KARI completed the conceptual design and conducted a System Requirements Review (SRR) while also initiating the design and upgrade of engine test facilities, the layout planning for the launch pad system, and the development of preliminary launch operation plans. In addition, to enhance the full-cycle technology development capabilities of the private sector and foster a private-led space industry ecosystem, a prime contractor will be selected to participate in development from the design stage. The next-generation launch vehicle is scheduled to perform three key missions: a lunar orbit injection performance verification launch in 2030, a lunar soft landing verification launch in 2031, and the final lunar lander model launch in 2032.
The launch pad development for the next-generation launch vehicle will proceed by fully rebuilding Launch Pad 1, which was previously used for the launches of Naro-1 and the engine test launch vehicles for NURI. The site has been selected after evaluating the necessary scale of facilities, including the enlargement of ground mechanical structures, modifications to the flame deflector design, and expansion of launch control and propellant supply systems to support next-generation launch vehicle operations. The new launch pad will comprise ground mechanical systems, propellant supply systems, and launch control systems, with certification expected by 2030.
Ground Mechanical Systems | Launch pad (including flame deflector), launch vehicle hold-down device, erector, transporter-erector, launch vehicle transport system, first-stage and upper-stage umbilical connection devices, umbilical tower |
---|---|
Propellant Supply Systems | Cryogenic systems (oxidizer/nitrogen supply systems), fuel supply systems (fuel supply and residual fuel recovery systems), gas supply systems (high-pressure gas production/supply systems, electro-hydraulic panels), temperature control systems, safety systems (flame deflector cooling, launch vehicle protection, oxygen concentration monitoring) |
Launch Control Systems | Ground equipment power supply system, ground equipment control system, ground equipment parameter measurement system, system cabling and instrumentation, launch control infrastructure |