Engineering:1.5KS35000

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1.5KS35000
Solid-fuel motor
Country of origin	United States
Designer	Thiokol
Status	Retired
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]

References

↑ McDowell, Jonathan (February 2007). "Stages". http://www.planet4589.org/space/lvdb/sdb/Stages. Retrieved 2010-03-02.
↑ 1.5KS35000

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Rocket engines