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     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:
    T is the combustion chamber temperature. 
        Te is the exhaust temperature.
        Is is the specific impulse.