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Designer: Isayev. Developed in: 1955-60. Application: P-15 Termit. Propellants: Nitric acid/Amine Thrust(vac): 1,213 kgf. Thrust(vac): 11.90 kN. Chambers: 1. Country: Russia. Status: Out of Production. References: 342 , 344 . Comments: Designation unknown. Thrust range 11.895-5.43 kN.
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Last update 12 March 2001.
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