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r = propellant burning rate n = steady-state burning rate pressure exponent, r pp = propellant density PDL = low-pressure stable deflagration limit M = average molecular weight of gaseous combustion products Tf = adiabatic flame temperature of propellant Tg = a temperature parameter that is approximated by the adiabatic flame temperature of the ammonium perchlorate monopropellant flame kg = rate constant for the ammonium perchlorate monopropellant flame reactions, kg = Ag exp(—Eg/RTg)
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Robert F. Chaiken (1965) studied this question.
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