RS-68 Regen
Designer: Rocketdyne. Developed in: 2005. Propellants: Lox/LH2. Chambers: 1. Country: USA. Status: Design concept -2004.

Upgrade to basic RS-68 for Delta IV Heavy growth versions. Details not specificed, except that it would use a regeneratively-cooled expansion nozzle, presumably allowing it to run hotter, higher thrust and specific impulse.  
 
 
 
 
 
 
 
 


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