15D25
Designer: KBMash. Developed in: 1961-1966. Application: RT-2 Stage 3. Propellants: Solid. Thrust(vac): 137.000 kN (30,798 lbf). Diameter: 0.98 m (3.21 ft). Length: 3.83 m (12.56 ft). Chambers: 1. Country: Russia. Status: Out of Production.

Three gimballed nozzles for steering. Ammonium perchlorate/aluminium propellant.  
 
 
 
 
 
 
 
 

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