1.9KS2150
From Wikipedia, the free encyclopedia
| 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.
- ↑ Wade, Mark (2008). "Judi". Archived from the original on December 29, 2008. Retrieved 2010-03-14.
- ↑ [[http://planet4589.org/jcm/jmcdowell.html|McDowell, Jonathan]] (February 2007). "Stages". Retrieved 2010-03-14.
This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.