Engineering:1.9KS2150
From HandWiki
Short description: Solid propellant rocket engine
 | This article appears to be a dictionary definition. |
| 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. https://web.archive.org/web/20090101211159/http://www.astronautix.com/engines/19ks2150.htm. Retrieved 2010-03-14.
- ↑ Wade, Mark (2008). "Judi". Archived from the original on December 29, 2008. https://web.archive.org/web/20081229221539/http://www.astronautix.com/stages/judi.htm. Retrieved 2010-03-14.
- ↑ McDowell, Jonathan (February 2007). "Stages". http://www.planet4589.org/space/lvdb/sdb/Stages. Retrieved 2014-04-16.
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