The thermal effects of incident radiation on the burning characteristi
cs of homogeneous solids are considered and the practical implications
of these effects in solid rocket motors are assessed. The applicabili
ty of the equivalence principle (equivalence between radiation and ini
tial temperature) is investigated experimentally and analytically. Exp
erimental steady burning rates asa function of initial temperature and
mean radiant flux are presented for a fine ammonium perchlorate (AP)
composite propellant which indicate that the equivalence principle is
accurate to within experimental error. The equivalence principle is al
so assessed analytically by considering the worst case conditions of c
ondensed phase controlled burning. For deflagration and pyrolysis of s
olids controlled by condensed phase reactions it is shown that a modif
ica; tion of Ibiricu and Williams' high activation energy asymptotic b
urning rate expression allows consideration of the effect of incident
radiation on steady burning rate over a wide range of propellant opaci
ties. Numerical simulations are used to verify this modification. Ther
mal radiation from combustion gases in typical non-metalized solid roc
ket motors is examined using band model calculations. These calculatio
ns show that even pure molecular gas radiation (no particles) can reac
h near blackbody levels for realistic motor conditions. The effects of
thermal radiation on burning rate and temperature sensitivity are als
o examined using the equivalence principle. It is shown that differenc
es in burning rare and temperature sensitivity between motors and prop
ellant strands which in the past have primarily been attributed to ero
sive burning, could in some instances be due to thermal gas radiation.
The implications of gas radiation on combustion stability are also di
scussed. It is shown that radiation may have either a stabilizing or d
estabilizing effect, according to the initial temperature dependence o
f the temperature sensitivity sigma(p)-(T-0), although in most cases i
t is a stabilizing influence.