1.9KS2150

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1.9KS2150
Country of origin United States
Designer RPI
Status Retired
Solid-fuel motor
Performance
Thrust (vac.) 9 kN
Dimensions
Length 1.70 m
Diameter 0.08 m


1.9KS2150 is a solid propellant rocket engine designed by RPI and used in some stages of the Cajun Dart, Deacon and Loki rockets. It was used in at least 617 launches.[1][2][3]

References[edit]

  1. ^ Wade, Mark (2008). "1.9KS2150". Archived from the original on January 1, 2009. Retrieved 2010-03-14. 
  2. ^ Wade, Mark (2008). "Judi". Archived from the original on December 29, 2008. Retrieved 2010-03-14. 
  3. ^ McDowell, Jonathan (February 2007). "Stages". Retrieved 2014-04-16.