SRM-2
Manufacturer Name: Orbus 6. Designer: CSD. Gross Mass: 3,919 kg (8,639 lb). Empty Mass: 1,170 kg (2,570 lb). Propellants: Solid. Thrust(vac): 78.400 kN (17,625 lbf). Thrust(sl): 51.600 kN (11,600 lbf). Isp: 304 sec. Isp (sea level): 200 sec. Burn time: 103 sec. Diameter: 1.61 m (5.28 ft). Length: 2.08 m (6.82 ft). Chambers: 1. Country: USA. First Flight: 1982. Last Flight: 2005. Flown: 58.

Used in Shuttle, Titan 34D; IUS-2. Known by manufacturer as Orbus 6.


SRM-2 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