TX-261-3

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Engine Model: TX-261-3. Designer: Thiokol. Propellants: Solid. Thrust(vac): 244.000 kN (54,853 lbf). Burn time: 11 sec. Diameter: 0.71 m (2.32 ft). Length: 3.10 m (10.10 ft). Country: USA. TX-261-3 used on Rocket Stages Used on stage: Pedro. on launch vehicle: Athena RTV. Used on stage: Pedro. on launch vehicle: Recruit. Used on stage: TX-261. on launch vehicle: ARPAT. 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.