1.5KS35000

From Wikipedia, the free encyclopedia
Jump to: navigation, search
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[edit]

  1. ^ Wade, Mark (2008). "1.5KS35000". Retrieved 2010-03-02. 
  2. ^ McDowell, Jonathan (February 2007). "Stages". Retrieved 2010-03-02.