RD-0255

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

RD-0255

Part of RD-0228

RD-0255
Credit: KBKhA

Kosberg N2O4/UDMH rocket engine. R-36M2 / RS-20V (SS-18 Mod-4) stage 2. Comprises of single-chamber main engine RD-0256 plus four-chamber steering engines RD-0257. Development based on RD-0228 with thrust increase by 11%. First flight 1986.

Date: 1983-89. Number: 42 . Thrust: 755.00 kN (169,730 lbf).

Chambers: 1 + 4.

Family: Storable liquid. Country: Russia. Launch Vehicles: Dnepr. Propellants: N2O4/UDMH. Stages: R-36M2-2. Agency: Kosberg bureau. Bibliography: 309, 330, 342.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z