M-13 Designer: Nissan. Gross Mass: 34,800 kg (76,700 lb). Empty Mass: 7,640 kg (16,840 lb). Propellants: Solid. Thrust(vac): 1,262.400 kN (283,799 lbf). Thrust(sl): 1,142.400 kN (256,822 lbf). Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 70 sec. Diameter: 1.41 m (4.62 ft). Length: 14.75 m (48.39 ft). Chambers: 1. Country: Japan. First Flight: 1969. Last Flight: 1995. Flown: 24. M-13 used on Rocket Stages Used on stage: Mu-3S-1. on launch vehicle: Mu-3.                   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 - 2007 except where otherwise noted.

Encyclopedia Astronautica topic index 0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z Enter your search terms   Web www.astronautix.com Submit search form