Nuri (Korean:누리;lit.'world'), also known as KSLV-II (Korean Space Launch Vehicle-II), is an expendable, three-stage-to-orbit, small-lift launch vehicle, the second one developed by South Korea, and the successor to Naro-1 (KSLV-1) It is developed by Korea Aerospace Research Institute (KARI). All three stages use Korean developed launch vehicle engines, making Nuri the first orbital launch vehicle entirely developed and manufactured in South Korea.
History
The South Korean government decided to fund the development of relatively cheap and reliable rockets competitive enough for the commercial launch market.
On 21 October 2021, Nuri made its initial orbital launch attempt at 08:00 UTC and it launched a 1,500kg (3,300lb) dummy satellite payload into what was planned to be a 700km (430mi)Sun-synchronous orbit (SSO). However, despite the payload reaching the targeted apogee (700km), the third stage shut down about 46 seconds earlier than planned and the payload did not achieve orbital speed.
Nuri made its second flight on 21 June 2022, 07:00 UTC, with a payload of 1,500kg (3,300lb) including a 1,300kg (2,900lb) dummy satellite payload and a 180kg (400lb) performance verification satellite (PVSAT) including four cube satellites. The second launch was successful, putting all the satellites onto the 700km (430mi)Sun-synchronous orbit (SSO). As a result of this launch, South Korea became the seventh country in the world with the ability to put a satellite with a mass of at least one ton, into orbit.
After the two test launches, Nuri showed higher than expected performance, increasing its payload from 1,500kg (3,300 Ib) to 1,900kg (4,200 Ib).
Nuri is the first launch vehicle developed with domestic, South Korean, technology throughout all processes, including design, manufacturing, and testing. With its successful launch, South Korea became the seventh country in the world to have a medium-sized liquid-propellant rocket engine over 75 tons.
Nuri (KSLV-II) is a three-stage launch vehicle. The first stage booster uses four KRE-075 SL engines generating 266.4 tons of thrust with a specific impulse of 289.1 seconds. The second stage booster uses a single KRE-075 Vacuum engine, which has a wider nozzle for increased efficiency in vacuum with a specific impulse of 315.4 seconds. The third stage booster uses one KRE-007 engine with a specific impulse of 325.1 seconds. Both engine models use Jet A-1 as fuel and liquid oxygen (LOX) as oxidizer.
Development
When technology development for Nuri began by October 2010, the overall design goal was to develop a new expendablemedium-liftlaunch vehicle that was entirely South Korean. Nuri first reached orbit in June 2022. The total cost of the development program was approximately US$1.5 billion.
In March 2014, the first combustion test of the 7-ton class combustor, was successfully completed, and the total assembly and initial ignition test of the KRE-007 engine started in July 2015. In addition, the first phase of the project was completed with the addition of a three-stage engine combustion test facility and a combustor combustion test facility. However, the problem of combustion instability in the KRE-075 burner required rework.
The third launch on 25 May 2023
Hanwha Techwin Co. signed on 25 January 2016, a 14.1 billion won (US$11.77 million) contract with the Korea Aerospace Research Institute (KARI) to produce both types of liquid propellant rocket engines for Nuri.
On 8 January 2016, the second phase of the project was carried out to overcome the difficulties of combustor combustion instability and welding technology of the liquid engine fuel tank, and a combustion test of the KRE-075 engine for a few seconds was successful.
On 3 May 2016, the KRE-075 engine underwent a 1.5 second long spark ignition test. It was later fired for 75 seconds on 8 June 2016. Following these successes, on 20 July 2016, at 1:39 pm, the final target combustion time of 145 seconds (147 seconds) was achieved. During the ground test, the engine performed nominally, with all values such as combustion safety and combustion thrust within the expected error range. During an actual launch, the first stage engine is expected to burn for 127 seconds and the second stage engine for 143 seconds.
Starting from October 2016 to October 2021, there have been over 184 combustion tests of the second prototype KRE-075 engine.
The KRE-075 engine was developed in April 2016 after the 30 tf engine development program.
KRE-075 vacuum engine
Fuel
Jet A-1 / LOX
Thrust
3,570kN (803,000lbf)
Specific impulse
315.4s (3.093km/s)
Cycle
Gas generator
KRE-007 engine
Fuel
Jet A-1 / LOX
Thrust
310kN (70,000lbf)
Specific impulse
325.1s (3.188km/s)
Cycle
Gas generator
KSLV-II TLV
The Test Launch Vehicle (TLV) was a single stage launch vehicle (with a planned two stage version), qualifying the performance of the KRE-075 engine which powers the KSLV-II. The TLV was 25.8m (85ft) in length, 2.6m (8ft 6in) in diameter, and with a mass of 52.1 tons. The main-stage liquid rocket propellant engine was fully gimballed. With the 2nd stage engine installed, the two-stage version of TLV could perform as a small satellite launch vehicle.
2018 flight
Wet Mass
52.1 tons
Dry Mass
38 tons
Height
25.8 m
Diameter
2.6 m
Stages
1
Engine
1 KRE-075
Payload
mass simulator
The TLV was launched from the Naro Space Center in Goheung, South Jeolla Province, on 28 November 2018. The main objective of the first suborbital flight was for the single-stage rocket's main engine to burn 140 seconds, reaching a 100km altitude before splashing down in the sea between Jeju Island and Okinawa Island.
The maiden flight was first delayed from 25 October 2018 for one month, due to abnormal readings detected in the launch vehicle propellant pressurization system. The test flight was then rescheduled for 28 November 2018, at 07:00 UTC (16:00 KST). No payload was to be placed into orbit.
The launch of the TLV while deemed successful with its main engine burning for 151 seconds in a 10-minute flight, was not broadcast live. After reaching a maximum altitude of 209km (130mi), the launch vehicle stage splashed down in the Pacific Ocean, 429km (267mi) southeast of Jeju Island.
As the TLV was meant to serve as a test craft, and as the flight ended in a success, there was not a second TLV launch.
Canceled future version (KSLV-IIA)
As of 2020, further improvements were planned to be added after the success of KSLV-II program, under the name of KSLV-IIA. With mainly increasing the thrust of the KRE-075 of the first stage from 735kN (165,000lbf) to 804kN (181,000lbf) and specific impulse from 261.7 seconds to 315.4 seconds, this would have increased the capacity of a payload to 700km SSO to increase from 1900kg to 2200kg. The overall size of the rocket was also planned to grow, to the height of 54m and wet mass of 232 tons.
Nuri will be used in launching several Earth observation satellites, such as KOMPSAT, medium-class satellites and LEO reconnaissance satellites. It is planned to support South Korea's Moon exploration mission to send orbiters and landers. Nuri will be South Korea's first launch vehicle to enter the commercial launch service market. The launch cost is estimated to be around US$30 million, which is cheaper than its Asian counterparts. This will allow for South Korea to provide cheap launch services for Southeast Asia countries.
South Korea plans to launch a high-weight rocket named KSLV-3 in 2030 instead of improving the KSLV-2. The decision is aimed at narrowing the technology gap with other countries.
Instead, it plans to develop a low-cost rocket that miniaturizes the KSLV-2 and is considering launching a military satellite to monitor North Korea.
↑Under the Roscosmos classification. It would be a medium-lift launch vehicle under the NASA classification.
References
↑"한국 토종 우주발사체 누리호는 300개 기업이 함께 만들고 있다"[South Korea's homegrown space launch vehicle, Nuri, is being built through the collaboration of 300 companies.]. dongascience.donga.com (in Korean). 25 February 2021. Retrieved 26 February 2021.
↑"국내 기술로 독자 개발 중인 한국형발사체 누리호 공개"[Nuri, the Korean launch vehicle being independently developed with domestic technology, unveiled.]. Korean Ministry of Science and Technology Information and Communication (in Korean). 19 January 2020. Retrieved 26 February 2021.
↑"2조 규모의 '차세대발사체(KSLV-III)' 개발 사업, 예타 조사 통과"[2-Trillion-Won 'Next-Generation Launch Vehicle (KSLV-III)' Development Project Passes Feasibility Study]. sanhak (in Korean). 29 November 2022. Retrieved 23 January 2023.
↑"[출처: 중앙일보] 설계부터 제작까지 100% 국산 로켓 내달 발사"[[Source: JoongAng Ilbo] 100% domestically produced rocket—from design to manufacturing—to launch next month.] (in Korean). JoongAng Ilbo. 7 September 2018. Retrieved 7 September 2018.
↑Ayeong, Kim (22 June 2022). "다가온 '뉴 스페이스' 시대‥"민간에 누리호 기술 이전""[The 'New Space' Era Is Here... "Nuri Rocket Technology to Be Transferred to the Private Sector"] (in Korean). MBC News. Retrieved 24 June 2022.
1234"[누리호] 설계부터 1차 발사까지 11년 7개월의 일지"[[Nuri] A Timeline of 11 Years and 7 Months: From Design to the First Launch] (in Korean). Science Times. 22 October 2021. Archived from the original on 24 June 2022. Retrieved 24 June 2022.
↑[KARI]연비가 향상된 로켓엔진 연소시험(100초) 공개[[KARI] Combustion Test (100 Seconds) of Rocket Engine with Improved Fuel Efficiency Revealed] (in Korean). Korea Aerospace Research Institute KARI TV. 6 December 2018. Archived from the original on 18 November 2021. Retrieved 7 February 2019– via YouTube.
↑Korea Aerospace Research Institute [@kari2030] (10 September 2018). "올 10월로 다가올 #시험발사체 조립 장면 타임랩스 영상으로 만나 보시죠!"[Check out this time-lapse video showing the assembly of the test launch vehicle, scheduled for launch this October!] (Tweet) (in Korean). Retrieved 7 February 2019– via Twitter.
↑"사진 > KARI IMAGE"[picture > KARI IMAGE]. kari.re.kr (in Korean). Retrieved 7 February 2019.
↑Korea Aerospace Research Institute [@kari2030] (13 November 2018). "11월 28일, 한국형발사체 '누리호'의 엔진시험을 위한 시험발사체 발사가 추진될 예정입니다"[On November 28, a test launch vehicle is scheduled to be launched to test the engine of Nuri, the Korean launch vehicle.] (Tweet) (in Korean). Retrieved 7 February 2019– via Twitter.
↑Korea Aerospace Research Institute [@kari2030] (27 November 2018). "#시험발사체 발사 성공! 발사 모습을 영상으로 공개합니다"[#TestLaunchVehicle launch successful! We are releasing a video of the launch.] (Tweet) (in Korean). Retrieved 7 February 2019– via Twitter.
↑2020년도 예비타당성조사 보고서 한국형발사체 고도화 사업[2020 Preliminary Feasibility Study Report on the Korean Launch Vehicle Upgrade Project](PDF) (Report) (in Korean). Korea Institute of S&T Evaluation and Planning (KISTEP). 23 August 2021. Retrieved 25 October 2025.
↑Min-gu, Kang (5 July 2021). "[일문일답]임혜숙 "예타 탈락 누리호 개량 사업 보완해 도전""[[Q&A] Lim Hye-sook: "We Will Revise and Resubmit the Nuri Upgrade Project After Preliminary Feasibility Study Rejection"]. Edaily (in Korean). Retrieved 25 October 2025.
↑Gu-hui, Jeong (30 October 2021). "[더스페셜리스트] 가성비 떨어지는 누리호? 그래도 쏴야 하는 이유"[[The Specialist] Is Nuri Not Cost-Effective? Here's Why We Must Launch It Anyway]. SBS news (in Korean). Retrieved 4 May 2022.
This template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future
Symbol † indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)