86 results on '"Itouyama, Noboru"'
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2. Wave-converging pressure increase in curved cylindrical rotating detonation combustors
3. The circumferential force on a cylindrical rotating detonation engine
4. Visualization and thrust measurement of rotating detonation engine with various channel expansion angles
5. Impact of mixture mass flux on hydrodynamic blockage ratio and Mach number of rotating detonation combustor
6. Experimental study on detonation-diffraction reflection point distances in hydrogen and gaseous hydrocarbon reactive systems
7. Investigation of reflective shuttling detonation cycle by schlieren and chemiluminescence photography
8. Analysis of Dispersibility Effect of Carbon Additives on Ignitability of Ammonium-Dinitramide-Based Ionic Liquid Propellants Using Continuous Wave Laser Heating.
9. Lagrangian dispersion and averaging behind a two-dimensional gaseous detonation front
10. Technical Report of The Research Activity for High Energy Materials (2022)
11. Measurement of In-situ Image, Temperature, and Current of ADN-based Ionic Liquids Voltage-applied
12. Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine
13. Conceptual Design of Small-Sized Thruster Using Laser Ignition of High-Energy Monopropellant
14. Investigation of Fundamental Operating Characteristics of Laser Radiation Heating Ignited Thrusters Using High-Energetic Ionic Liquid Propellant
15. Experimental Study on Initiating Detonation Waves by Shock Focusing in Laser Ignition
16. Experimental Research on Internal Flow Structure of Cylindrical Rotating Detonation Engine Using Ethanol
17. In-space Demonstrations of Rotating Detonation Engines: from Gaseous Propellant to Liquid Propellant Applications
18. Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31 in Space
19. Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-31
20. Visualization and Performance Evaluation of a Liquid-Ethanol Cylindrical Rotating Detonation Combustor
21. Flight Demonstration Experiment of Liquid Propellant Detonation Engine System Using Sounding Rocket S-520-34
22. Technical Report of The Research Activity for High Energy Materials (2021)
23. Research of High Energetic Ionic Liquid Propellants for Micro Propulsion System
24. Experimental investigation of inner flow of a throatless diverging rotating detonation engine.
25. New HAN-based mixtures for reaction control system and low toxic spacecraft propulsion subsystem: Thermal decomposition and possible thruster applications
26. Experimental investigation of inner flow of a throatless diverging rotating detonation engine
27. A Concept of the Small Chemical Thruster with High Energetic Ionic Liquids
28. Analysis of Dispersibility Effect of Carbon Additives on Ignitability of Ammonium-Dinitramide-Based Ionic Liquid Propellants Using Continuous Wave Laser Heating
29. Supersonic Exhaust from a Rotating Detonation Engine with Throatless Diverging Channel
30. Analysis of Parent/Nitrated Polycyclic Aromatic Hydrocarbons in Particulate Matter 2.5 Based on Femtosecond Ionization Mass Spectrometry
31. Technical Report of the Research Activity for Innovative Micro Propulsion Systems for Future Deep Space Explorations (2020)
32. Study on Innovative Micro-Propulsion System Technologies for Micro-Space Probes
33. Technical Report of The Research Activity for High Energy Materials (2020)
34. Research of High Energetic Ionic Liquid Propellants for Future Space Applications
35. Experimental Research on Thrust Performance of Rotating Detonation Engine with Liquid Ethanol and Gaseous Oxygen
36. Development of an S-Shaped Pulse Detonation Engine for a Sounding Rocket
37. Cylindrical Rotating Detonation Engine with Propellant Injection Cooling
38. 観測ロケットS-520 31号機プロジェクト デトネーションエンジンシステムの宇宙動作実証結果
39. Flight Demonstration Experiment of Liquid Propellant Detonation Engine System Using Sounding Rocket S-520
40. S-520-31号機によるデトネーションエンジンシステムの宇宙実験 -設計・試験・運用の概要-
41. S-520-31号機によるデトネーションエンジンシステムの宇宙実験 -実験結果報告とサクセスクライテリア評価-
42. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude
43. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: History from Development to Flight
44. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine
45. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: System Design
46. Experimental Clarification on Detonation Phenomena of Liquid Ethanol Rotating Detonation Combustor
47. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Pulse Detonation Engine
48. Effect on dispersibility of carbon-absorbents heated by CW laser in liquids
49. 高エネルギーイオン液体推進剤の点火システムの研究開発
50. Fundamental-Computing Investigation for Detonation on Gas-Phase of High Energetic Materials
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