| Country of origin United States Status Retired Length 2.60 m | Designer Thiokol Thrust (vac.) 156 kN Diameter 0.23 m | |
 | ||
1.5KS35000 is a solid propellant rocket engine designed by Thiokol and used in the experimental Recruit rocket. It was used in at least 23 launches.
References
1.5KS35000 Wikipedia(Text) CC BY-SA