1.9KS2150

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1.9KS2150
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

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  2. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  3. ↑ Lua error in package.lua at line 80: module 'strict' not found.


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