KEW-1 Credit: Boeing / Rocketdyne |
Date: 1988. Thrust: 29 N (7 lbf). Specific impulse: 266 s.
KEW-3 Rocketdyne N2O4/MMH rocket engine. Kinetic Energy Propulsion (100 lb thrust). Pressure-fed. ASAT Strap-down test, XSS / DICE Microsatellite, GBI Ground-Based Interceptor, THAAD Theater High Altitude Area Defense. |
KEW-2 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. |
KEW-4 Rocketdyne N2O4/MMH rocket engine. Kinetic Energy Propulsion (500 lb thrust). Pressure-fed. ASAT Strap-down test, XSS / DICE Microsatellite, GBI Ground-Based Interceptor, THAAD Theater High Altitude Area Defense. |