1.5KS35000

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

↑ Wade, Mark (2008). "1.5KS35000". Retrieved 2010-03-02.
↑ McDowell, Jonathan (February 2007). "Stages". Retrieved 2010-03-02.

Non-military suborbital rocket engines and motors that have flown

Liquid fuel engines	BE-3 Ofen-B WAC Corporal XLR10 XLR99

Hybrid Propellant Engines	RocketMotorOne RocketMotorTwo

Solid Propellant Motors	1.5KS35000 Algol X-254 Altair Aerobee Alcor Asp Black Brant Castor Genius Improved Orion Malemute Orion Oriole Rohini S-20 S-30 S-31 S40TM S44M S-310 S-520 Talos Terrier

Related articles	Sub-orbital spaceflight Sub-orbital tourism Sounding rocket

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