1.9KS2150

Summary

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]

1.9KS2150
Country of originUnited States
DesignerRPI
StatusRetired
Solid-fuel motor
Performance
Thrust, vacuum9 kN
Dimensions
Length1.70 m
Diameter0.08 m

ReferencesEdit

  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". Archived from the original on 2003-10-23. Retrieved 2014-04-16.