Method and Apparatus for Reducing Smoke at Launch of High Performance Rockets.
DEPARTMENT OF THE NAVY WASHINGTON D C
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The patent application relates to a method whereby the exhaust signature of high performance rockets is reduced by including in a solid propellant rocket motor a substantially smokeless, double-base propellant and a smoky, high-energy, composite propellant, both simultaneously ignited during missile launch.
- Combustion and Ignition
- Solid Propellant Rocket Engines
- Solid Rocket Propellants