| Country of origin | USSR |
|---|---|
| First flight | 1981-12-27[1] |
| Designer | OKB-154[1] |
| AssociatedLV | RSM-54,Shtil'[1] |
| Status | Retired |
| Liquid-fuel engine | |
| Propellant | N2O4[1] /UDMH[1] |
| Mixture ratio | 2.6[2] |
| Cycle | Oxidizer Rich Staged combustion[1] |
| Configuration | |
| Chamber | 1[2] |
| Performance | |
| Thrust | 682 kilonewtons (153,000 lbf)[2] |
| Chamberpressure | 27.5 megapascals (3,990 psi)[2] |
| Specific impulse, vacuum | 310 s (3.0 km/s)[2] |
| Specific impulse, sea-level | 280 s (2.7 km/s)[2] |
| Burn time | 74 seconds[2] |
| Used in | |
| RD-0243 Propulsion Module[3] | |
| Country of origin | USSR |
|---|---|
| First flight | 1981-12-27[1] |
| Designer | OKB-154[1] |
| AssociatedLV | RSM-54,Shtil'[1] |
| Status | Retired |
| Liquid-fuel engine | |
| Propellant | N2O4[1] /UDMH[1] |
| Mixture ratio | 2.6[4] |
| Cycle | Gas Generator[1] |
| Configuration | |
| Chamber | 4[4] |
| Nozzle ratio | 14 |
| Performance | |
| Thrust | 211 kilonewtons (47,000 lbf)[4] |
| Chamberpressure | 14.7 megapascals (2,130 psi)[4] |
| Specific impulse, vacuum | 300 s (2.9 km/s)[4] |
| Specific impulse, sea-level | 280 s (2.7 km/s)[4] |
| Burn time | 79 seconds[4] |
| Used in | |
| RD-0243 Propulsion Module[3] | |
TheRD-0243 (Russian:Ракетный Двигатель-0243,romanized: Raketnyy Dvigatel-0243,lit. 'Rocket Engine 0243') is a propulsion module composed of anRD-0244 main engine and aRD-0245vernier thruster. Both areliquid-fuel rocket engines, burning ahypergolic mixture ofunsymmetrical dimethylhydrazine (UDMH) fuel withdinitrogen tetroxide (N2O4) oxidizer. TheRD-0244 main engine operates in theoxidizer rich staged combustion cycle, while thevernierRD-0245 uses the simplergas generator cycle. Since volume is at a premium on submarine launches, this module is submerged on the propellant tank.[3] Its development period was from 1977 to 1985, having had its first launch on December 27, 1981. Originally developed for theRSM-54, it was used later for theShtil'.[1]
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