## Richard Nakka's Experimental Rocketry Web Site

### Derivation of equation describing chamber pressure due to igniter charge From the ideal gas law, pressure within the chamber may be expressed as Introducing the term G relating the fraction of igniter charge burned at any time t, and considering that the initial chamber pressure is ambient letting ("effective force") gives which may be rewritten as letting (loading fraction) gives multiply numerator and denominator by r (charge density) since , this gives where:

P = pressure in combustion chamber at time, t    lbf/in2

r= density of charge material    lbm/in3

C = original mass of charge    lbm

V = free volume of combustion chamber at time, t    in3

l = R T/ M "effective force" (energy),     in-lbf /lbm

R = universal gas constant    in-lbf /° R-lbm

M = effective molecular weight of combustion products (system mass divided by number of moles of gas)    lbm / mole

T = adiabatic flame temperature    ° R

G = fraction of original charge mass consumed by time, t    dimensionless

Pa = atmospheric pressure    lbf/in2

Note that the assumption is made that combustion of the igniter charge occurs rapidly with no pressure loss due to gas seepage through the nozzle opening.
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