S-23

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Engine Model: S-23. Designer: Avibras. Gross Mass: 200 kg (440 lb). Empty Mass: 69 kg (152 lb). Propellants: Solid. Thrust(vac): 18.000 kN (4,046 lbf). Burn time: 20 sec. Diameter: 0.30 m (0.98 ft). Length: 2.20 m (7.20 ft). Country: Brazil. S-23 used on Rocket Stages Used on stage: Sonda II. on launch vehicle: Sonda. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.