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 | | Status 1996 was RD-120 prototype with 1.8 m diam., development estimated for three years.",1,794 - 873,1433, 1.50, 2.80, 163 - 172,,LOX/Kerosene,334 - 336,295 - 298,,2.6,Russia,IAF-97-S.1.03 RD-134,,,upper stage,NPO Energomash,,"Proposed upper stage kerosene engine. |
 | | Nozzle expansion ratio is 120/0.05=2400.",1,19.6,129, 0.76, 1.70, 117.7, 351.6,LOX/Kerosene,380.6,0,900,3.69,Russia,IAF-97-S.1.03 RD-161 (1),,,Soyuz M stage 3,NPO Energomash,1993-,"Basic version of upper stage kerosene engine. |
 | | Nozzle expansion ratio is 120/0.05=2400.",1,19.6,124, 0.76, 1.70, 117.7, 351.6,LOX/Kerosene,360,0,900,2.6,Russia,"Energomash 93, IAF-97-S.1.03" RD-161 (2),,,Soyuz M stage 3 (block LM),NPO Energomash,1993-,Version with uncooled nozzle extension,1,19.9,141, 1.02, 2.21, 117.7, 370.6,LOX/Kerosene,365,0,900,2.6,Russia,Energomash 93 RD-161P,,,Soyuz M stage 3 (block LM),NPO Energomash,1993-,Version for H2O2 fuel. |
| www.friends-partners.org /partners/mwade/articles/ruseng3.csv (6745 words) |
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