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Burning-rate behavior in aluminized wide-distribution AP composite propellants
M. Q. Brewster
, J. C. Mullen
Mechanical Science and Engineering
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Physics & Astronomy
composite propellants
99%
ammonium perchlorates
97%
burning rate
86%
flames
39%
propellants
37%
particulates
33%
laminates
30%
polybutadiene
28%
matrices
24%
aluminum
22%
flame interaction
17%
burn-in
15%
Peclet number
13%
premixed flames
13%
heat sinks
13%
pressure dependence
11%
slabs
9%
exponents
8%
scalars
7%
heat
7%
Engineering & Materials Science
Composite propellants
100%
Propellants
53%
Polybutadienes
47%
Laminates
44%
Peclet number
22%
Feedback
20%
Heat sinks
17%
Fluxes
13%
Hot Temperature
7%
Chemical Compounds
Propellant
80%
Flame
57%
Pressure
38%
Peclet Number
26%
Premixed Flame
24%
Slab Like Crystal
18%
Heat
12%
Mixture
7%
Amount
7%