H1500
Propellants: Lox/Solid. Thrust(vac): 931.300 kN (209,365 lbf). Thrust(sl): 928.000 kN (208,622 lbf). Isp: 284 sec. Isp (sea level): 283 sec. Burn time: 75 sec. Diameter: 1.83 m (6.00 ft). Chambers: 1. Country: USA. Status: Design 1988.


H1500 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