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RD R-29R (1)
Part of RD-0243
Makeyev N2O4/UDMH rocket engine.

Thrust: 682.00 kN (153,319 lbf). Burn time: 74 s.



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: Volna-1. Agency: Makeyev bureau.

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