1 - 13 |
Electrical sensitization studies in the initiation of liquid propellant 1846 Sturman PC, Woodmansee DE |
14 - 16 |
Detonation pressure of donors as a parameter for assessing detonation transfer probabilities Tzidony D, Jaeger M |
17 - 22 |
Behaviour of a working fluid in an electrothermal launcher chamber Baschung B, Samirant M, Zimmerman K, Steinbach C, Mura D |
23 - 27 |
Theoretical studies on the mechanism of hydrolysis of nitroguanidine by AMI method Xiao HM, Li YM, Li YF |
28 - 33 |
Concept and performance of a non-azide propellant for automotive airbag inflators Hara K, Yoshida T, Misawa T, Maekawa T, Yoshi S, Yokoyama T, Kazumi T, Hayashi M |
34 - 42 |
Electrostatic discharge ignition of energetic materials Skinner D, Olson D, Block-Bolten A |
43 - 45 |
The evaluation of activation energies through the hot plate test Underhill PR, Bardon MF |
46 - 47 |
Synthesis of 2-methyl-2-nitro-1-azidopropane Wang NX, Li JS, Chen BR, Ou YX |
48 - 49 |
A study of beta-azidoethylamino-3-nitro-1,2,4-triazole-5-onate Dong SA, Chen BR, Ou YX, Pan ZL |
50 - 55 |
A convenient correlation for prediction of binary eutectics involving organic explosives Chapman RD, Fronabarger JW |
56 - 60 |
Analysis of stabilizer degradation products in propellants using HPLC and photodiode away (PDA) detection Oehrle SA |