Status: Out of Production. Date: 1958-63. Thrust: 392.00 kN (88,125 lbf).
Chambers: 4. Propellant Formulation: AK27I/TG-02.
S5.3M Isayev Nitric acid/Amine rocket engine. R-9 (SS-8) missile stage 1. Out of Production. Proposed for R-9 missile stage 1. Four engines per stage. 396,7 kN sea-level. |