Claims:

  1. Use of shear line areas to determine peak pressure and pressure as a function of time throughout cartridge burn.

  2. Use of propellant compression data at first bullet movement to determine shear line length. Definition of the texture term "T" and its effect on chamber pressure in the burn area equation.
  3. Use of the dO and dI terms to determine maximum pressure as a function of burn time.

  4. Use of the lO and lI terms to determine burn areas.

  5. Recognition of the burn area equation and how it changes as a function of time.

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