7 - 8 |
Advanced Processing - The Changing Face of Manufacturing Cumming AS |
9 - 19 |
CFD and Experimental Analysis of Swirl Type Single-fluid Atomizer for Optimization of Recrystallization Process to make Ultrafine RDX Explosive Goyal V, Gupta S, Kumar PD, Jindal D, Singh G, Agarwal A, Lata P |
20 - 25 |
Process Optimization of Supercritical CO2 Foamed SF-3 Double-Base Propellant Tan DQ, Wei XA, Zhang D, Chen FY, He WD, Wang ZS |
26 - 35 |
Rheological Considerations for Binder Development in Direct Ink Writing of Energetic Materials Woods H, Boddorff A, Ewaldz E, Adams Z, Ketcham M, Jang DJ, Sinner E, Thadhani N, Brettmann B |
36 - 52 |
Development of Propellant Compositions for Vat Photopolymerization Additive Manufacturing Straathof MH, van Driel CA, van Lingen JNJ, Ingenhut BLJ, ten Cate AT, Maalderink HH |
53 - 76 |
An Assessment of Printing Methods for Producing Two-Dimensional Lead-Free Functional Pyrotechnic Delay-Lines for Mining Applications BelL TM, Williamson DM, Walley SM, Morgan CG, Kelly CL, Batchelor L |
77 - 86 |
Resonant Acoustic (R) Mixing: Processing and Safety Andrews MR, Collet C, Wolff A, Hollands C |
87 - 91 |
Comparison of Propellant Processing by Cast-Cure and Resonant Acoustic Mixing Zebregs M, Mayer AEHJ, van der Heijden AEDM |
92 - 100 |
Application and Properties of CL-20/HMX Cocrystal in Composite Modified Double Base Propellants Wu ZK, Liu N, Zheng W, Chen JB, Song XD, Wang JN, Cui C, Zhang DX, Zhao FQ |
101 - 111 |
The Preparation and Rheological Properties of Novel Energetic Composites TEGDN/NBC Huang XR, Luo QP, Zhu J, Li ZQ, Li CZ, Pei CH |
112 - 117 |
Generating Plateau Burning Segments for Composite Solid Rocket Propellants El-Basuony SA, Sadek MA, Wafy TZ, Mostafa HE |
118 - 127 |
Equivalent Principle of Time-Temperature-Strain Rate for Poisson's Ratio of Composite Solid Propellant Lv X, Zhou WY, Shen ZB, Cui HR |
136 - 140 |
Study on the Fracture Properties of HTPB Propellant at Low Temperature Long B, Wang HL, Gao SS |
141 - 146 |
Influence of MnO2 and Fe2O3 on the Burning Characteristics of AN/AP-based Composite Propellants Kohga M, Togo S |
154 - 154 |
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