RD-134R

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RD-134R

Part of RD-134

Glushko LOx/Kerosene rocket engine. Angara stage 2 vernier. Design concept 1993-on. Proposed in initial study for Angara by RKK Energia in1993. Steering engines for Angara upper stage. Kerosene RG-1.

Status: Design concept 1993-on. Date: 1993. Thrust: 343.00 kN (77,109 lbf).

Chambers: 4 (?).

Country: Russia. Propellants: Lox/Kerosene. Agency: Glushko bureau.

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