Status: Out of Production. Date: 1958-63. Thrust: 392.00 kN (88,125 lbf).
Chambers: 4. Propellant Formulation: AK27I/TG-02.
Subtopics 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. Family: Storable liquid. Country: Russia. Launch Vehicles: R-21. Propellants: Nitric acid/Amine. Agency: Isayev bureau. Bibliography: 319, 320, 343, 344. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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