AJ-260X

Manufacturer Name: AJ-260X. Designer: Aerojet. Gross Mass: 1,648,355 kg (3,634,000 lb). Empty Mass: 156,126 kg (344,198 lb). Propellants: Solid. Thrust(vac): 35,390.700 kN (7,956,146 lbf). Thrust(sl): 32,026.700 kN (7,199,889 lbf). Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 114 sec. Diameter: 6.60 m (21.60 ft). Length: 30.48 m (99.99 ft). Chambers: 1. Country: USA. Status: Study 1967.

Proposed for use in various Saturn and Nova configurations. Full length version of 260 inch motor tested in 1960's.

AJ-260X used on Rocket Stages

Used on stage: 260 inch solid FL. on launch vehicle: MLLV.

Used on stage: 260 inch solid FL. on launch vehicle: Saturn INT-05A.

Used on stage: 260 inch solid FL. on launch vehicle: Saturn V-D.

Used on stage: 260 inch solid FL. on launch vehicle: Saturn V/4-260.

Used on stage: MLLV-0.

Used on stage: Saturn LCB-SR. on launch vehicle: Saturn LCB-SR.

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