1.9KS2150
 | This article appears to be a dictionary definition. |
| Country of origin | United States |
|---|---|
| Designer | RPI |
| Status | Retired |
| Solid-fuel motor | |
| Performance | |
| Thrust, vacuum | 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.
- ^ Wade, Mark (2008). "Judi". Archived from the original on December 29, 2008. Retrieved 2010-03-14.
- ^ McDowell, Jonathan (February 2007). "Stages". Archived from the original on 2003-10-23. Retrieved 2014-04-16.
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- Rocket engines
- Rocketry stubs