1.5KS35000
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1.5KS35000
| Country of origin | United States |
|---|---|
| Designer | Thiokol |
| Status | Retired |
| Solid-fuel motor | |
| Performance | |
| Thrust (Vac.) | 156 kN |
| Dimensions | |
| Length | 2.60 m |
| Diameter | 0.23 m |
1.5KS35000 is a solid propellant rocket engine designed by Thiokol and used in the experimental Recruit rocket. It was used in at least 23 launches.[1][2]
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References
- ^ Wade, Mark (2008). "1.5KS35000". http://www.astronautix.com/engines/15k35000.htm. Retrieved 2010-03-02.
- ^ [|McDowell, Jonathan] (Feb. 2007). "Stages". http://www.planet4589.org/space/lvdb/sdb/Stages. Retrieved 2010-03-02.
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