Associated Engines

RD0257 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2 vernier. Out of Production. Steering engine of system RD0255. Gas generator cycle. First flight 1987. More...

RD0255 Kosberg N2O4/UDMH rocket engine. 755 kN. R36M2 / RS20V (SS18 Mod4) stage 2. Comprises of singlechamber main engine RD0256 plus fourchamber steering engines RD0257. Development based on RD0228 with thrust increase by 11%. First flight 1986. More...

RD0256 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2. Out of Production. Main engine of system RD0255. Staged combustion cycle. First flight 1987. More...

RD869 Yuzhnoye N2O4/UDMH rocket engine. 8.580 kN. R36M2 vehicle bus. Based on RD864. Two thrust levels. The four thrusters swing out of the stage housing before use. Chamber pressure 41 / 17 bar. Diameter 3,0 / 4,02 m. Isp=313s. First flight 1986. More...
Associated Launch Sites

Dombarovskiy Headquarters of an RVSN Division, 1964present. Operated 64 heavy ICBM silos (R36/R36M). One silo was modified to launch surplus R36M missiles as orbital launch vehicles, and used for used for 3 launches from 2004 to 2007. More...
Associated Engines

RD0257 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2 vernier. Out of Production. Steering engine of system RD0255. Gas generator cycle. First flight 1987. More...

RD0255 Kosberg N2O4/UDMH rocket engine. 755 kN. R36M2 / RS20V (SS18 Mod4) stage 2. Comprises of singlechamber main engine RD0256 plus fourchamber steering engines RD0257. Development based on RD0228 with thrust increase by 11%. First flight 1986. More...

RD0256 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2. Out of Production. Main engine of system RD0255. Staged combustion cycle. First flight 1987. More...

RD869 Yuzhnoye N2O4/UDMH rocket engine. 8.580 kN. R36M2 vehicle bus. Based on RD864. Two thrust levels. The four thrusters swing out of the stage housing before use. Chamber pressure 41 / 17 bar. Diameter 3,0 / 4,02 m. Isp=313s. First flight 1986. More...
Associated Launch Sites

Dombarovskiy Headquarters of an RVSN Division, 1964present. Operated 64 heavy ICBM silos (R36/R36M). One silo was modified to launch surplus R36M missiles as orbital launch vehicles, and used for used for 3 launches from 2004 to 2007. More...
Associated Engines

RD0257 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2 vernier. Out of Production. Steering engine of system RD0255. Gas generator cycle. First flight 1987. More...

RD0255 Kosberg N2O4/UDMH rocket engine. 755 kN. R36M2 / RS20V (SS18 Mod4) stage 2. Comprises of singlechamber main engine RD0256 plus fourchamber steering engines RD0257. Development based on RD0228 with thrust increase by 11%. First flight 1986. More...

RD0256 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2. Out of Production. Main engine of system RD0255. Staged combustion cycle. First flight 1987. More...

RD869 Yuzhnoye N2O4/UDMH rocket engine. 8.580 kN. R36M2 vehicle bus. Based on RD864. Two thrust levels. The four thrusters swing out of the stage housing before use. Chamber pressure 41 / 17 bar. Diameter 3,0 / 4,02 m. Isp=313s. First flight 1986. More...
Associated Launch Sites

Dombarovskiy Headquarters of an RVSN Division, 1964present. Operated 64 heavy ICBM silos (R36/R36M). One silo was modified to launch surplus R36M missiles as orbital launch vehicles, and used for used for 3 launches from 2004 to 2007. More...
Associated Engines

RD0257 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2 vernier. Out of Production. Steering engine of system RD0255. Gas generator cycle. First flight 1987. More...

RD0255 Kosberg N2O4/UDMH rocket engine. 755 kN. R36M2 / RS20V (SS18 Mod4) stage 2. Comprises of singlechamber main engine RD0256 plus fourchamber steering engines RD0257. Development based on RD0228 with thrust increase by 11%. First flight 1986. More...

RD0256 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2. Out of Production. Main engine of system RD0255. Staged combustion cycle. First flight 1987. More...

RD869 Yuzhnoye N2O4/UDMH rocket engine. 8.580 kN. R36M2 vehicle bus. Based on RD864. Two thrust levels. The four thrusters swing out of the stage housing before use. Chamber pressure 41 / 17 bar. Diameter 3,0 / 4,02 m. Isp=313s. First flight 1986. More...
Associated Launch Sites

Dombarovskiy Headquarters of an RVSN Division, 1964present. Operated 64 heavy ICBM silos (R36/R36M). One silo was modified to launch surplus R36M missiles as orbital launch vehicles, and used for used for 3 launches from 2004 to 2007. More...
Associated Engines

RD0257 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2 vernier. Out of Production. Steering engine of system RD0255. Gas generator cycle. First flight 1987. More...

RD0255 Kosberg N2O4/UDMH rocket engine. 755 kN. R36M2 / RS20V (SS18 Mod4) stage 2. Comprises of singlechamber main engine RD0256 plus fourchamber steering engines RD0257. Development based on RD0228 with thrust increase by 11%. First flight 1986. More...

RD0256 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2. Out of Production. Main engine of system RD0255. Staged combustion cycle. First flight 1987. More...

RD869 Yuzhnoye N2O4/UDMH rocket engine. 8.580 kN. R36M2 vehicle bus. Based on RD864. Two thrust levels. The four thrusters swing out of the stage housing before use. Chamber pressure 41 / 17 bar. Diameter 3,0 / 4,02 m. Isp=313s. First flight 1986. More...
Associated Launch Sites

Dombarovskiy Headquarters of an RVSN Division, 1964present. Operated 64 heavy ICBM silos (R36/R36M). One silo was modified to launch surplus R36M missiles as orbital launch vehicles, and used for used for 3 launches from 2004 to 2007. More...
Associated Engines

RD0257 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2 vernier. Out of Production. Steering engine of system RD0255. Gas generator cycle. First flight 1987. More...

RD0255 Kosberg N2O4/UDMH rocket engine. 755 kN. R36M2 / RS20V (SS18 Mod4) stage 2. Comprises of singlechamber main engine RD0256 plus fourchamber steering engines RD0257. Development based on RD0228 with thrust increase by 11%. First flight 1986. More...

RD0256 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2. Out of Production. Main engine of system RD0255. Staged combustion cycle. First flight 1987. More...

RD869 Yuzhnoye N2O4/UDMH rocket engine. 8.580 kN. R36M2 vehicle bus. Based on RD864. Two thrust levels. The four thrusters swing out of the stage housing before use. Chamber pressure 41 / 17 bar. Diameter 3,0 / 4,02 m. Isp=313s. First flight 1986. More...
Associated Launch Sites

Dombarovskiy Headquarters of an RVSN Division, 1964present. Operated 64 heavy ICBM silos (R36/R36M). One silo was modified to launch surplus R36M missiles as orbital launch vehicles, and used for used for 3 launches from 2004 to 2007. More...
Associated Engines

RD0257 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2 vernier. Out of Production. Steering engine of system RD0255. Gas generator cycle. First flight 1987. More...

RD0255 Kosberg N2O4/UDMH rocket engine. 755 kN. R36M2 / RS20V (SS18 Mod4) stage 2. Comprises of singlechamber main engine RD0256 plus fourchamber steering engines RD0257. Development based on RD0228 with thrust increase by 11%. First flight 1986. More...

RD0256 Kosberg N2O4/UDMH rocket engine. R36M2 / RS20V (SS18 Mod4) stage 2. Out of Production. Main engine of system RD0255. Staged combustion cycle. First flight 1987. More...

RD869 Yuzhnoye N2O4/UDMH rocket engine. 8.580 kN. R36M2 vehicle bus. Based on RD864. Two thrust levels. The four thrusters swing out of the stage housing before use. Chamber pressure 41 / 17 bar. Diameter 3,0 / 4,02 m. Isp=313s. First flight 1986. More...
Associated Launch Sites

Dombarovskiy Headquarters of an RVSN Division, 1964present. Operated 64 heavy ICBM silos (R36/R36M). One silo was modified to launch surplus R36M missiles as orbital launch vehicles, and used for used for 3 launches from 2004 to 2007. More...