1.5KS35000
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| Country of origin | United States |
|---|---|
| Designer | Thiokol |
| Status | Retired |
| Solid-fuel motor | |
| Performance | |
| Thrust, vacuum | 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]
References
- ^ McDowell, Jonathan (February 2007). "Stages". Retrieved 2010-03-02.
- ^ 1.5KS35000
Non-military suborbital rocket engines and motors that have flown | ||
|---|---|---|
| Liquid fuel engines |  | |
| Hybrid propellant engines | ||
| Solid propellant motors | ||
| Related articles | ||
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