AKA: Zenit C-0. Status: Retired 1989. Thrust: 80.00 kN (17,984 lbf). Gross mass: 200 kg (440 lb). Burn time: 4.00 s. Height: 1.00 m (3.20 ft). Diameter: 0.44 m (1.44 ft).
RO solid rocket engine. Zenit C zero stage.