A methodology for developing gas-phase reaction mechanisms for nitrami
ne propellants is discussed. Examples of Fundamental kinetic experimen
ts and detailed modeling calculations are given that emphasize a hiera
rchical construction procedure for both the types of experiments neces
sary for collecting kinetic: data and the specific chemical submodels
that need to be studied. In particular, three kinetic submodels of inc
reasing complexity are described with selected results from flow react
or experiments. With kinetic data generated from these experiments and
others, chemical submodels are developed and validated by comparison
of model predictions with experimental measurements using reaction flu
x and sensitivity analyses to guide the process. Collectively, the sub
models, validated over the entire range of experimentally studied cond
itions, are assembled to form the gasphase nitramine combustion mechan
ism. Because of the nature of the developmental procedure, e.g,, the n
ecessity for different types of experiments, ranging from ''microscopi
c'' measurements of isolated reaction rate constants to ''macroscopic'
' studies on kinetic mechanisms in flames, the process is inherently i
terative. As an example of this iterative procedure, numerical results
are presented on the ignition behavior of hexahydro-1,3,5-trinitro-1,
3,5-triazine (RDX) after updating a previously developed model with re
cent results from submodel validation experiments, These results show
changes in the pathways of many secondary species involved in RDX deco
mposition.