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%

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Reaction Products Nozzleof aluminized AP composite propellants composed of FOX-7

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CO2 (g) H2O (g) N2 (g) CO (g) H2 (g) Al2O3 (s) C (s)

5% 10% 15% 20% 25% 30% 35%

40% 45% 50% 55% 60% 65% 70%

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2100

2200

2300

2400

2500

2600

2700

0 10 20 30 40 50 60 70 80

% nitro-compounds

I sp [

Ns/k

g]

FOX-7 TNAZ CL-20 NTO HMX

!"#$&(#$P4!#%C#(%24,0-!(&1(#&24&-!+(&1('%$*&@#&24&,'+-Q(D%'+!*@=RST(30@=LST(3M.@(ALURS<

!%Theoretical thermodynamic combustion properties of composite propellants

1,6

1,62

1,64

1,66

1,68

1,7

1,72

1,74

1,76

FOX-7 TNAZ CL-20 HMX NTO

nitro-compounds

density,

g/c

m3

5% 35% 70%

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