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ZIF-IR-189
Solid propellant rocket stage. . Used monolithic single motor with Nylon-S propellant. Combustion chamber pressure 30-40 kg/cm2.

Gross mass: 5,850 kg (12,890 lb). Unfuelled mass: 1,150 kg (2,530 lb). Specific impulse: 220 s. Specific impulse sea level: 220 s. Diameter: 1.80 m (5.90 ft). Span: 1.80 m (5.90 ft).



Country: Russia. Launch Vehicles: Variant S. Propellants: Solid.

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