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Rotary Rocket
XCOR LOx/Kerosene rocket engine. First stages. Developed in 1990's. Developed and tested by Rotary Rocket for their launcher before its cancellation.

Status: Developed in 1990's. Date: 2000-2004. Thrust: 22.25 kN (5,002 lbf).

In April 2002, XCOR acquired selected intellectual property assets of the former Rotary Rocket Company. These assets included a 22,250-newton LOX/kerosene engine developed and tested by the company as well as hydrogen peroxide engine technology.



Country: USA. Propellants: Lox/Kerosene. Agency: XCOR.

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