Dissertation　

About 290 item dissertation in line with Propellant query results,the following is 1 to 50(Search took 0.022 seconds)

  1. Research on Measuring Method of Adhesive Thickness of Solid Propellant Grain Surface by the Grating Projection,ShiBingHua/University of North,0/1
  2. Applicability of a Natural Swelling Matrix Stemed from Boat-fruited Sterculia Seed as Propellant of Osmotic Pump Tablets,WuLi/Anhui University of Chinese Medicine,0/14
  3. Study on Thermal Analysis, Ignition and Combustion Characteristics of AP/HTPB Base Bleed Propellant,ShenHui/Nanjing University of Technology and Engineering,0/11
  4. Mechanical Response Analysis of Cylindrical Shell with Visco-elastic Liner,MaXiaoWei/Harbin Institute of Technology,0/17
  5. Optimal Design and Experiment of100mN Hall Effect Thrusters,QiaoZengXi/Harbin Institute of Technology,0/13
  6. Under complex loading solid rocket motor charge of stress relief groove optimization design,PengChao/Nanjing University of Technology and Engineering,0/14
  7. Synthesis and Applications of Modified Boric Acid Ester Bonding Agents,PengJie/Hunan University,0/0
  8. Preliminary Study on the Combustion Performance of Al-based Alloy Powder and Research on Reaction of Al-H2O via Electrochemical Technology,ZuoDaMing/Huazhong University of Science and Technology,0/24
  9. Investigation of the Burning Behaviour of Aluminum-ice Solid Propellants,HanXiuJie/Harbin Engineering University,0/47
  10. Study on Combustion Characteristics and Two-Phase Flow of the Base-Bleed Aluminized Composite Propellant,GuoXiLiang/Nanjing University of Technology and Engineering,0/7
  11. Hydrogen peroxide gel atomization and two staged combustion characteristic research,ChenJie/Nanjing University of Technology and Engineering,0/16
  12. Propellant micro mechanical bonding interface model and parameter acquiring method research,WeiZhen/Nanjing University of Technology and Engineering,0/14
  13. Research on the Thermo-visco-hyperelastic Constitutive Model of NEPE Propellant Over a Large Range of Strain Rates,ZhangJunFa/Nanjing University of Technology and Engineering,0/19
  14. Preparation of HMX/Cu Composite Partcle by Electroless Plating Method and Its Performances Study,XiongLu/Nanjing University of Technology and Engineering,0/4
  15. Study on overload parameter test method of solid propellants,FanHui/Nanjing University of Technology and Engineering,0/18
  16. Study on the Recycling and Particle Size Controlling of AP from Retired Composite Propellant,ZhangXiaoHui/Nanjing University of Technology and Engineering,0/19
  17. Numerical Simulation Research on the Single-screw Extrusion Process of Propellant Substitute,YinShuPan/Nanjing University of Technology and Engineering,0/6
  18. Study on the Preparation and Charging Technology of Smokeless Propellant for Fireworks Based on Low-grade NC,JiaZuoYu/Nanjing University of Technology and Engineering,0/6
  19. Experimental study of ordered with supercritical fluid heterogeneous nuclear pore orientation,SuPeng/Nanjing University of Technology and Engineering,0/4
  20. Numerical Simulation on the Extrusion Process of Propellant Based on POLYFLOW,WangZuo/Nanjing University of Technology and Engineering,0/17
  21. Study on burning rate propellant factor parameter test evaluation method and its influence,WangJunJie/Nanjing University of Technology and Engineering,0/12
  22. Study on Synthesis, Characterization and Application of Ferrocene-Based Compounds and Ferrocene-Based Polymers and Their Grafted Carbon Materials,GaoJingMin/Zhejiang University,0/119
  23. Multibody Dynamic Modeling and Simulation of Liquid-Propellant Launch Vehicles,HuPengXiang/Tsinghua University,0/36
  24. Research of the Propellant Grain X-ray Real-time Imaging and Processing System,WangShiQin/University of North,1/26
  25. Study on High Energy Propellant Based on Energetic Thermoplastic Elastomers,LiNing/Nanjing University of Technology and Engineering,0/18
  26. Recovery integrated air gun performance of emission,LiHuaLun/Nanjing University of Technology and Engineering,0/28
  27. Deformation and Stress Damage of Base Bleed Propellant under High Overload,ZhaoYaMan/Nanjing University of Technology and Engineering,0/42
  28. Numerical Simulation of Liquid Traveling Charge of Spray Atomization and Combustion,WangChunLei/Nanjing University of Technology and Engineering,0/28
  29. Optimization Design and Numerical Simulation on Interior Ballistics of Regenerative Liquid Propellant Gun,JuXiaoZuo/Nanjing University of Technology and Engineering,0/15
  30. Experimental and Numerical Research on Thermo-Viscoelastic Constitutive Model of Composite Propellant,XuJinSheng/Nanjing University of Technology and Engineering,0/17
  31. Study on Yield Criteria and Visco-elastoplastic Constitutive Model of the Double-base Propellant,ZhangJianBin/Nanjing University of Technology and Engineering,0/13
  32. The Study of Functional Additives for the Water Ramjet Engine Propellant,TanXiaoLei/Hunan University,0/31
  33. Study on grain large strain measurement method,RuanXiaoFeng/Nanjing University of Technology and Engineering,1/37
  34. Study on the mechanical response of temperature impact load of grain,YueXiaoLiang/Nanjing University of Technology and Engineering,0/68
  35. Study on Combustion Gas Flow and Spreading Laws of the Double-base Propellant Fire in Confined Space,TangWeiWei/Nanjing University of Technology and Engineering,0/34
  36. Attenuation Performance of Pyrotechnic to the IR Signal of HTPB Composite Propellant,ZhengTingTing/Nanjing University of Technology and Engineering,0/56
  37. Study of Extraction Ammonium Perchorate from Solid Composite Propellants,WangJun/Nanjing University of Technology and Engineering,0/70
  38. Influence of Nano-CuO Dispersibility on the Combustion of Solid Propellant,YuXinJie/Nanjing University of Technology and Engineering,0/62
  39. The Analysis on Crack Growth of Solid Propellant,LvZhi/Harbin Institute of Technology,0/15
  40. Characteristics of composite propellant crack flow and combustion,GongLunKun/Nanjing University of Technology and Engineering,0/21
  41. Research on Measurement System of Solid Propellant Kneading Machine’s Temperature and Pressure,ChenSong/Xi'an University of Technology,0/45
  42. Preparation and Properties of DB/AP/Al Incendiary Agent,LiuXiangLing/Nanjing University of Technology and Engineering,0/46
  43. Research and application of mechanics models of double base propellant at high strain rate,WangPengBo/Nanjing University of Technology and Engineering,0/50
  44. Aluminum magnesium alloy metal fuel preparation and thermal characteristics of reaction,JiaChongLei/Nanjing University of Technology and Engineering,0/58
  45. Study on the Fracture Mechanics Behavior of Solid Rocket Motor Propellant Containing Defects,ZhouGuangPan/Nanjing University of Technology and Engineering,0/66
  46. A New Method of Study Mg/Ptfe Fuel Rich Propellant Formula Optimization Design Adopt ANN and GA,FanLei/Nanjing University of Technology and Engineering,0/77
  47. Development of solid propellant overloading parameters testing system based on FPGA,QuBingBing/Nanjing University of Technology and Engineering,0/65
  48. Research on Microstructural Damage and Its Numerical Simulation Method for Composite Solid Propellant,ChangWuJun/Nanjing University of Technology and Engineering,0/86
  49. Different materials on the study of RDX coated surface,ZhongHuaJie/Nanjing University of Technology and Engineering,0/97
  50. Continuous measurement and process research of online storage group,ZhangJun/Nanjing University of Technology and Engineering,0/34

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