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According to the Korea Aerospace Research Institute (KARI), Nuri (누리호) is a three-stage liquid-propellant launch vehicle designed to “directly put a 1.5-ton application satellite into a 600-800 km Sun-synchronous orbit”. The first stage consists of four clustered 75-ton engines, the second stage has one 75-ton engine, and the third stage features a one 7-ton engine. In the first flight test, Nuri (also known as Korea Space Launch Vehicle-2 or KSLV-II) failed to place the dummy satellite into the target orbit due to a premature shutdown of the third-stage engine. On the second test launch, Nuri will try to place a dummy payload (1500 kg) into a Sun-synchronous orbit.
Credit: Korea Aerospace Research Institute (KARI)