353 - 359 |
Estimated Detonation Velocities for TKX-50, MAD-X1, BDNAPM, BTNPM, TKX-55, and DAAF using the Laser-induced Air Shock from Energetic Materials Technique Gottfried JL, Klapotke TM, Witkowski TG |
360 - 369 |
Research on Feasibility of Several High Density Materials for EFP Liner and Material Selection Criteria Ding L, Jiang JW, Men JB, Wang SY, Li M |
370 - 375 |
Direct Detection of Triacetone Triperoxide (TATP) in Real Banknotes from ATM Explosion by EASI-MS Correa DN, Melendez-Perez JJ, Zacca JJ, Borges R, Schmidt EM, Eberlin MN, Meurer EC |
376 - 380 |
An Efficient Method for Determination of the Diphenylamine (Stabilizer) in Propellants by Molecularly Imprinted Polymer based Carbon Paste Electrochemical Sensor Hande PE, Samui AB, Kulkarni PS |
381 - 385 |
Smokeless GAP-RDX Composite Rocket Propellants Containing Diaminodinitroethylene (FOX-7) Jensen TL, Unneberg E, Kristensen TE |
386 - 393 |
Isocyanate-Free Curing of Glycidyl Azide Polymer with Bis-propargylhydroquinone Sonawane S, Anniyappan M, Athar J, Singh A, Talawar MB, Sinha RK, Banerjee S, Sikder AK |
394 - 400 |
Effect of Bonding Agent on the Mechanical Properties of GAP High-Energy Propellant Deng JK, Wang XQ, Li GP, Luo YJ |
401 - 409 |
Evaluation of 4-(Dimethylsilyl) Butyl Ferrocene Grafted HTPB as a Burning Rate Modifier in Composite Propellant Formulation using Bicurative System Kurva R, Gupta G, Dhabbe KI, Jawale LS, Kulkarni PS, Maurya M |
410 - 416 |
In-situ Characterization and Cure Kinetics in NEPE Propellant/HTPB Liner Interface by Microscopic FT-IR Gui DY, Zong YY, Ding S, Li CH, Zhang QL, Wang ML, Liu JH, Chi XH, Ma XG, Pang AM |
417 - 422 |
Effect of Organic Fluoride on Combustion Agglomerates of Aluminized HTPB Solid Propellant Zhou XY, Zou MS, Huang FL, Yang RJ, Guo XY |
423 - 429 |
Assessment of Physico-Thermal Properties, Combustion Performance, and Ignition Delay Time of Dimethyl Amino Ethanol as a Novel Liquid Fuel Pakdehi SG, Keshavarz MH, Akbari M, Ghorbani M |
430 - 437 |
Effect of Pre-strain Aging on the Damage Properties of Composite Solid Propellants based on a Constitutive Equation Zhou DM, Liu XY, Sui X, Wei ZJ, Wang NF |
438 - 447 |
Influence of Anvil Properties on RDX Thin Layer Ignition Behavior Yakaboski O, Kumar AV |