| 63 - 67 |
A gap test driven by optimality statistics software
Konig PJ, Mostert FJ |
| 68 - 72 |
Performance test results of an economical, high performance, melt castable IHE
Sumrall TS |
| 73 - 76 |
Reparametrization of the BKW equation of state for the triazoles and comparison of the detonation properties of HMX, TNMA and NTO by means of ab-initio and semiempirical calculations
Vaullerin M, Espagnacq A, Blaise B |
| 77 - 81 |
The interrelation between the thermal decomposition of lead salt and the platonization mechanism of double-base propellants
Yang D, Song HC, Li SW |
| 82 - 85 |
Characterization of the phase equilibrium of the system trinitrotoluene/carbon dioxide
Teipel U, Gerber P, Krause HH |
| 86 - 89 |
Thermodynamic analysis of combustion products at high temperature and pressure
Belov GV |
| 90 - 93 |
Realization of an eco-friendly solid propellant based on HTPB-HMX-AP system for launch vehicle applications
Muthiah R, Varghese TL, Rao SS, Ninan KN, Krishnamurthy VN |
| 94 - 104 |
A nonlinear viscoelastic theory for solid rocket propellants based on a cumulative damage approach
Duncan EJS, Margetson J |
| 105 - 110 |
Glass armour and shaped charge jets
Held M |
| 111 - 113 |
Stationary phases 45. Chromatographic separation of high energetic materials with C-60-fullerene stationary phase
Chang CS, Wen CH, Den TG |
