1.9KS2150

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

  1. ^ Wade, Mark (2008). "1.9KS2150". Archived from the original on January 01, 2009. http://web.archive.org/web/20090101211159/http://www.astronautix.com/engines/19ks2150.htm. Retrieved 2010-03-14. 
  2. ^ Wade, Mark (2008). "Judi". Archived from the original on December 29, 2008. http://web.archive.org/web/20081229221539/http://www.astronautix.com/stages/judi.htm. Retrieved 2010-03-14. 
  3. ^ [|McDowell, Jonathan] (Feb. 2007). "Stages". http://www.planet4589.org/space/lvdb/sdb/Stages. Retrieved 2010-03-14.