There are a number of shipboard situations where the unintentional burning
of missile propellant is a concern. Full-scale test programs have investiga
ted the phenomena associated with propellant fires. An existing computer fi
re model, FAST, was modified to account for fire phenomena specific to miss
ile propellant combustion. The modified computer program and the developed
missile propellant burning rate algorithm were exercised in blind predictio
ns of full-scale tests. Comparisons between the blind predictions and the t
est data are presented, (C) 2000 Elsevier Science Ltd. All rights reserved.