1.9KS2150
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| 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
- ↑ Wade, Mark (2008). "1.9KS2150". Archived from the original on January 1, 2009. Retrieved 2010-03-14. Unknown parameter
|url-status=ignored (help) - ↑ Wade, Mark (2008). "Judi". Archived from the original on December 29, 2008. Retrieved 2010-03-14. Unknown parameter
|url-status=ignored (help) - ↑ McDowell, Jonathan (February 2007). "Stages". Archived from the original on 2003-10-23. Retrieved 2014-04-16. Unknown parameter
|url-status=ignored (help)
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