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KEW-2
Part of KEW-1
KEW-2
KEW-2
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/MMH rocket engine. Kinetic Energy Propulsion (50 lb thrust). Pressure-fed. ASAT Strap-down test, XSS / DICE Microsatellite, GBI Ground-Based Interceptor, THAAD Theater High Altitude Area Defense.

Date: 1992. Thrust: 215 N (48 lbf). Specific impulse: 275 s.



Family: Storable liquid. Country: USA. Propellants: N2O4/MMH. Agency: Rocketdyne.

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