1.5KS35000

1.5KS35000
Country of origin United States
Designer Thiokol
Status Retired
Solid-fuel motor
Performance
Thrust (Vac.) 156 kN
Dimensions
Length 2.60 m
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.[1][2]

References

  1. ^ Wade, Mark (2008). "1.5KS35000". http://www.astronautix.com/engines/15k35000.htm. Retrieved 2010-03-02. 
  2. ^ [|McDowell, Jonathan] (Feb. 2007). "Stages". http://www.planet4589.org/space/lvdb/sdb/Stages. Retrieved 2010-03-02.