Calculations
By means of
VLW code , the detonation performance of high energy
density materials, common military explosives, fuel air explosives, and civil
industrial explosives, emulsion explosives, and combustion properties of
propellants are computed as follows:
Table 01 high energy density materials
Explosive
|
Composition
|
Density
(g/cm3)
|
Pc-j (Gpa)
|
Dc-j(km/s)
|
Tc-j(K)
|
Cal
|
Exp
|
Cal
|
Exp
|
Cal
|
HMX
|
C4H8N8O8
|
1.90
|
39.6
|
39.3
|
9.107
|
9.100
|
4840
|
HNB
|
C6N6O12
|
1.972
|
37.7
|
------
|
9.384
|
9.300
|
6087
|
CL-20
|
C6H6N12O12
|
2.10
|
49.8
|
(42.0)*
|
9.850
|
(9.400)*
|
5252
|
Note:
* the estimated valuation from NWC-TP-8020, 1989
|
Table 02 common military explosives
Explosive
|
Composition
|
Density (g/cm3)
|
Pc-j (Gpa)
|
Dc-j (km/s)
|
Tc-j (K)
|
Cal
|
Exp
|
Cal
|
Exp
|
Cal
|
RDX
|
C3H6N6O6
|
1.80
|
34.7
|
34.7
|
8.764
|
8.754
|
4909
|
TNT
|
C7H5N3O6
|
1.64
|
18.8
|
19.0
|
6.923
|
6.950
|
4095
|
PETN
|
C5H8N4O12
|
1.77
|
31.3
|
33.5
|
8.333
|
8.300
|
5.86
|
|
|
|
|
|
|
|
|
|
Table 03 fuel air explosives
Fuel
|
Composition
|
Density (g/cm3)
|
Pc-j (Gpa)
|
Dc-j (km/s)
|
Tc-j(K)
|
Cal
|
Exp
|
Cal
|
Exp
|
Cal
|
Exp
|
Methane (7.25%)
|
C1H5N11.8O3.0
|
1.12
〜10-3
|
1.809
|
1.780
|
1.873
|
1.837
|
2811
|
2717
|
Epoxy propane
(9.62%)
|
C3H6N29.78O9.0
|
1.26
〜10-3
|
2.111
|
2.106
|
1.847
|
1.826
|
2987
|
2930
|
Table 04 civil emulsion explosives
Explosives
|
Composition
|
Density
(g/cm3)
|
Pc-j(Gpa)
|
Dc-j(km/s)
|
Tcj(K)
|
Cal
|
Exp
|
Cal
|
Exp
|
Cal
|
RJ-52
|
C0.4919H5.923N1.811
|
1.11
|
6.613
|
-----
|
5.006
|
5.096
|
2624
|
EL105
|
C0.6118H5.788N1.923
O3.723Na0.1412
|
1.11
|
6.274
|
-----
|
4.757
|
4.700
|
2702
|
Table 05 Propellants
Name
|
Composition
|
Tc (K)
|
Te (K)
|
Is (S)
|
Cal.
|
Theory
|
Cal.
|
Theory
|
Cal.
|
Theory
|
HMX
|
C4H8N8O8
|
3419
|
3293
|
1543
|
1633
|
266.1
|
266.5
|
Complex
|
C12.3H24.6N15.8O24.5
CL0.70AL7.00
|
3848
|
3877
|
2277
|
2263
|
273.8
|
273.3
|
Note:
Tc is the combustion chamber
temperature.
Te is the exhaust temperature.
Is is the
specific impulse.
|