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Government Designation: 5D25. Other Designations: S5.44. Designer: Isayev. Developed in: 1964-65. Application: SAM-missile 5Ya24. Propellants: Nitric acid/Amine Thrust(vac): 18,000 kgf. Thrust(vac): 177.00 kN. Isp (sea level): 251 sec. Mass Engine: 124 kg. Diameter: 0.5 m. Length: 1.7 m. Chambers: 1. Area Ratio: 118.00. Country: Russia. Status: Out of Production. References: 320 , 342 . Comments: Could be throttled. 177-49 kN sea-level. Area ratio 118 - 44.
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Last update 12 March 2001.
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