KSR-3

Propellants: Lox/Kerosene. Thrust(sl): 122.500 kN (27,539 lbf). Burn time: 53 sec. Chambers: 1. Country: Korea South. Status: In development. First Flight: 2002. Last Flight: 2002. Flown: 1.00.

Pressure-fed indigenous design.

KSR-3 used on Rocket Stages

Used on stage: KSR-3. on launch vehicle: KSLV-I 2002.

Used on stage: KSR-3. on launch vehicle: KSLV-I 2002.

Used on stage: KSR-3. on launch vehicle: KSLV-II.

Used on stage: KSR-3. on launch vehicle: KSLV-III.

Used on stage: KSR-3. on launch vehicle: KSR-III.

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