Abstract

a = sonic velocity, fps A — area, ft Cp = specific heat, Btu/lbm-°R g = gravitational constant, 32.2 lbm-ft/lbf-sec H = total (stagnation) enthalpy, Btu/lbm / = conversion constant, 778 ft-lbf/Btu m = mass, Ibm M = angular momentum, ft-lbf-sec, or Mach number m — mass flow rate, Ibm/sec n = propellant burning rate pressure exponent r = radius, ft R( = gas constant, lbf-ft/lbm-°R R ) = chamber radius, ft T = temperature, °R V = velocity, fps 7 = specific heat ratio p — density, lbm/ft w = spin rate, rad/sec

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