Nome |
# |
Trade-Off Analysis of a New Liquid Rocket Engine, file e0c31c0d-d886-4599-e053-1705fe0aef77
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768
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Combustion Processes in Hybrid Rockets, file e0c31c0e-8c43-4599-e053-1705fe0aef77
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388
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An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization, file e0c31c0d-c1e9-4599-e053-1705fe0aef77
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257
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An Italian Network to Improve Hybrid Rocket Performance: Strategy and Results, file e0c31c0e-7465-4599-e053-1705fe0aef77
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204
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Aging of ADN Rocket Propellant Formulations with Desmophen-Based Elastomer Binder, file e0c31c0e-b97d-4599-e053-1705fe0aef77
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188
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Mechanically Activated Al/Mg Powders for Solid Rocket Propellants, file e0c31c0d-bfc8-4599-e053-1705fe0aef77
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170
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Characterization of ADN/GAP-Based and ADN/Desmophen-Based Propellant Formulations and Comparison with AP Analogues, file e0c31c0e-746a-4599-e053-1705fe0aef77
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163
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A Wide Characterization of Paraffin-based Fuels Mixed with Styrene-based Thermoplastic Polymers for Hybrid Propulsion, file e0c31c08-0e6e-4599-e053-1705fe0aef77
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159
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Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry, file 240c430c-007f-44cb-9af3-f74ad4663713
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155
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Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine, file e0c31c0e-2922-4599-e053-1705fe0aef77
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145
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Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation, file e0c31c0f-7168-4599-e053-1705fe0aef77
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137
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Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants, file e0c31c0d-bfca-4599-e053-1705fe0aef77
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136
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Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity, file e0c31c0c-d1c7-4599-e053-1705fe0aef77
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127
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An experimental investigation of convective heat transfer at evaporation of kerosene and water in the closed volume, file e0c31c0e-3e74-4599-e053-1705fe0aef77
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127
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Catalyst Screening for Ammonium Nitrate Oxidizer, file e0c31c0b-37a8-4599-e053-1705fe0aef77
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117
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Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel, file e0c31c0e-71fc-4599-e053-1705fe0aef77
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107
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Effect of mechanical activation on the reactivity of composites for flameless heaters, file e0c31c10-0f29-4599-e053-1705fe0aef77
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105
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A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization, file e0c31c11-014f-4599-e053-1705fe0aef77
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103
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Development of an intrusive technique for particles collection in rockets plume, file e0c31c0c-d1b8-4599-e053-1705fe0aef77
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102
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Iron oxide as solid propellant catalyst: A detailed characterization, file e0c31c0e-ac62-4599-e053-1705fe0aef77
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101
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Numerical and Experimental Investigation of a Lab-Scale Paraffin Motor with Swirled Injection of Gaseous Oxygen, file e46d01ea-178e-489c-9b2d-4d9ec6eef619
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99
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Particle Size in SRM Plume: Assessment of Collection Method, file e0c31c0d-bfcf-4599-e053-1705fe0aef77
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97
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Reduction of Solid Propellants Environmental Impact: Al-Mg Mechanically Activated Fuels and AP-PSAN Blends, file 4c4fbae4-7880-4e62-8437-61946c5921c5
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91
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An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization, file e0c31c0e-567f-4599-e053-1705fe0aef77
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90
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Aluminum powders: aging effects on metal content and thermogravimetry reactivity, file e0c31c0d-3fd9-4599-e053-1705fe0aef77
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82
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Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications, file e0c31c10-8fe8-4599-e053-1705fe0aef77
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79
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Towards High-Performing Paraffin-Based Fuels Exploiting the Armored Grain Concept, file 6def32d2-ec17-4117-9bd4-9aeffef7a538
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72
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Detailed Properties of Iron Oxide Solid Propellant Catalyst, file e0c31c0b-369d-4599-e053-1705fe0aef77
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70
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Space Debris Mitigation and Remediation: Perspectives of Affordable Hybrid Propulsion Implementations, file e0c31c0c-138a-4599-e053-1705fe0aef77
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68
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Role of Pressure and Aluminum Size in Solid Propellant CCP Generation, file e0c31c0b-39d8-4599-e053-1705fe0aef77
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65
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Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine, file 3c602eae-a011-41b0-a493-a218d99030b3
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59
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A method for mechanical activation of powders by means of balls, file e0c31c0f-575c-4599-e053-1705fe0aef77
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56
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Paraffin-based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization, file e0c31c0e-50e6-4599-e053-1705fe0aef77
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55
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Preliminary kinetic characterization of lithium-aluminum based hydrides for airbreathing propulsion, file e0c31c0e-0000-4599-e053-1705fe0aef77
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51
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A wide characterization of Paraffin-based Fuels Mixed with Styrene-based thermoplastic polymers for hybrid propulsion, file e0c31c11-095a-4599-e053-1705fe0aef77
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37
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Hydrogen Generation from Aluminum Composites Hydrolysis for Space Propulsion, file f607dc1e-b4ec-4893-96a6-4fad6a54ed9c
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36
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Aerospace Propulsion Research Activities at SPlab. Overview and Results, file e0c31c0e-6baf-4599-e053-1705fe0aef77
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13
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Preliminary kinetic characterization of lithium-aluminum based hydrides for airbreathing propulsion, file e0c31c0b-8c2a-4599-e053-1705fe0aef77
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10
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Iron oxide as solid propellant catalyst: A detailed characterization, file e0c31c0c-cff5-4599-e053-1705fe0aef77
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10
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Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation, file e0c31c0b-2fda-4599-e053-1705fe0aef77
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8
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Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems, file e0c31c09-3473-4599-e053-1705fe0aef77
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7
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A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion, file e0c31c0b-3b3c-4599-e053-1705fe0aef77
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7
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Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-Based Formulations, file e0c31c0e-7202-4599-e053-1705fe0aef77
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7
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An experimental investigation of convective heat transfer at evaporation of kerosene and water in the closed volume, file e0c31c0b-95d4-4599-e053-1705fe0aef77
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6
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Regression Rate and Combustion Efficiency in a Vortex-Flow Hybrid Rocket Engine, file e0c31c0e-69e2-4599-e053-1705fe0aef77
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6
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Characterization of ADN/GAP-Based and ADN/Desmophen-Based Propellant Formulations and Comparison with AP Analogues, file e0c31c08-1697-4599-e053-1705fe0aef77
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5
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Aging of ADN Rocket Propellant Formulations with Desmophen-Based Elastomer Binder, file e0c31c08-1d5f-4599-e053-1705fe0aef77
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5
|
Paraffin-based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization, file e0c31c0b-2c46-4599-e053-1705fe0aef77
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5
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Aging Effects on Nano-Sized Aluminum Reactivity, file e0c31c0b-3e7e-4599-e053-1705fe0aef77
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5
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Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response, file e0c31c0e-1acb-4599-e053-1705fe0aef77
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5
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An Italian Network to Improve Hybrid Rocket Performance: Strategy and Results, file e0c31c08-1e87-4599-e053-1705fe0aef77
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4
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Paraffin-Based Fuels For Hybrid Propulsion: Characterization Of Waxes And Its Blends, file e0c31c0a-325a-4599-e053-1705fe0aef77
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3
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Development of a Compact Hybrid Rocket Engine for Low-Cost In-Space Propulsion, file e0c31c0d-74c3-4599-e053-1705fe0aef77
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3
|
Experimental data from ramjet/scramjet combustion and numerical validation perspectives, file e0c31c0e-1f5c-4599-e053-1705fe0aef77
|
3
|
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry, file 685dec27-3def-4895-a081-e70f502309fe
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2
|
End-To-end Flight Test for Planetary Landing, an Unprecedented Approach in Europe, file e0c31c08-0cc4-4599-e053-1705fe0aef77
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2
|
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution, file e0c31c08-7e86-4599-e053-1705fe0aef77
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2
|
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion, file e0c31c09-3d68-4599-e053-1705fe0aef77
|
2
|
Effects of Aluminum Composites on the Regression Rates of Solid Fuels, file e0c31c09-86cd-4599-e053-1705fe0aef77
|
2
|
Paraffin-Based Solid Fuels Characterization and Effect of Their Properties on Entrainment Phenomena, file e0c31c09-86cf-4599-e053-1705fe0aef77
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2
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Combustion Properties of Aluminum-Based Oxidizer-Lean Propellants, file e0c31c0b-33bf-4599-e053-1705fe0aef77
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2
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Quasi-steady and Forced Transient Burning of a Vortex Flow Hybrid Motor, file e0c31c0b-369c-4599-e053-1705fe0aef77
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2
|
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine, file e0c31c0b-99fc-4599-e053-1705fe0aef77
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2
|
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity, file e0c31c0c-dca5-4599-e053-1705fe0aef77
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2
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Overview of a supersonic probe for solid propellant rocket CCP collection, file e0c31c0d-3c49-4599-e053-1705fe0aef77
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2
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Combustion Processes in Hybrid Rockets, file e0c31c0e-8ddf-4599-e053-1705fe0aef77
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2
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A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization, file e0c31c10-000f-4599-e053-1705fe0aef77
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2
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Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain, file e0c31c10-56c3-4599-e053-1705fe0aef77
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2
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Rheological and Mechanical Characterization of Hybrid Rocket Solid Fuels, file e0c31c07-e22f-4599-e053-1705fe0aef77
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1
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Aging of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements, file e0c31c08-1002-4599-e053-1705fe0aef77
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1
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Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion, file e0c31c08-6fc3-4599-e053-1705fe0aef77
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1
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Theoretical Analysis of Hydrides in Solid and Hybrid Rocket Propulsion, file e0c31c08-7798-4599-e053-1705fe0aef77
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1
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Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion, file e0c31c08-7c9b-4599-e053-1705fe0aef77
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1
|
Uncertainty Propagation in Post-Firing Analysis of SRM Internal Ballistics, file e0c31c09-3475-4599-e053-1705fe0aef77
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1
|
A Parametric Study of the Effect of Liquid Fuel Entrainment on the Combustion Characteristics of a Paraffin-Based Hybrid Rocket Motor, file e0c31c09-86cc-4599-e053-1705fe0aef77
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1
|
Experimental Visualizations of Entrainment Phenomena in Wax-Based Fuels for Hybrid Space Propulsion, file e0c31c09-86d1-4599-e053-1705fe0aef77
|
1
|
Experimental Investigation of Solid Fuels for Hybrid Rocket Propulsion, file e0c31c09-86d3-4599-e053-1705fe0aef77
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1
|
Paraffin-Based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization, file e0c31c09-94d1-4599-e053-1705fe0aef77
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1
|
Vortex combustion in a hybrid rocket motor, file e0c31c09-e25e-4599-e053-1705fe0aef77
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1
|
Isothermal Two-Fluid Based CFD of Solid-Liquid Slush Flows for Propulsion Systems, file e0c31c0a-ec2f-4599-e053-1705fe0aef77
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1
|
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Conceptual and Detailed Design, file e0c31c0b-33c0-4599-e053-1705fe0aef77
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1
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Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Application of Quasi-1D Engineering Model and 2D Axisymmetric CFD, file e0c31c0b-3462-4599-e053-1705fe0aef77
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1
|
Numerical Simulation of Vortex Combustion in a Hybrid Rocket Motor, file e0c31c0b-3e80-4599-e053-1705fe0aef77
|
1
|
Development of an intrusive technique for particles collection in rockets plume, file e0c31c0c-d1b7-4599-e053-1705fe0aef77
|
1
|
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion, file e0c31c0d-ae3c-4599-e053-1705fe0aef77
|
1
|
Performance and Environmental Impact Prediction of SRMs. Road Map for Reliable Dataset of Particles in Plume, file e0c31c0e-715a-4599-e053-1705fe0aef77
|
1
|
Particle Size in Solid Rocket Motor Plume: New Experimental Method, file e0c31c0e-89e2-4599-e053-1705fe0aef77
|
1
|
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications, file e0c31c10-9643-4599-e053-1705fe0aef77
|
1
|
Actualization of an efficient throttleable laser propulsion mode, file e0c31c11-31e5-4599-e053-1705fe0aef77
|
1
|
Totale |
5.027 |