280 inch solid
Propellants: Solid. Thrust(vac): 46,208.000 kN (10,387,971 lbf). Isp: 265 sec. Isp (sea level): 238 sec. Burn time: 118 sec. Diameter: 7.10 m (23.20 ft). Length: 52.80 m (173.20 ft). Chambers: 1. Country: USA. Status: Study 1963.

Operational date would have been February 1973

280 inch solid used on Rocket Stages

 
 
 
 
 
 
 
 
 
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