Solid Propellant Measurement System.
Patent, Filed 10 Aug 81, patented 18 Oct 83,
DEPARTMENT OF THE NAVY WASHINGTON DC
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An apparatus for measuring the burning rate of solid propellants utilizes a homodyne radar to illuminate the propellant grain from a non-burning surface to obtain a distance measurement of the dimensions of the burning mass.
- Solid Rocket Propellants
- Combustion and Ignition