X-248 Manufacturer Name: X-248. Other Designations: Altair 1. Designer: Thiokol. Gross Mass: 238 kg (524 lb). Empty Mass: 30 kg (66 lb). Propellants: Solid. Thrust(vac): 12.400 kN (2,788 lbf). Thrust(sl): 11.300 kN (2,540 lbf). Isp: 256 sec. Isp (sea level): 233 sec. Burn time: 38 sec. Diameter: 0.46 m (1.50 ft). Length: 1.83 m (6.00 ft). Chambers: 1. Country: USA. First Flight: 1959. Last Flight: 1969. Flown: 51. X-248 used on Rocket Stages Used on stage: Altair 1. on launch vehicle: Atlas Able. Used on stage: Altair 1. on launch vehicle: Blue Scout 2. Used on stage: Altair 1. on launch vehicle: Delta. Used on stage: Altair 1. on launch vehicle: Delta A. Used on stage: Altair 1. on launch vehicle: Delta B. Used on stage: Altair 1. on launch vehicle: Delta C. Used on stage: Caleb-2. on launch vehicle: Caleb.                   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