IP. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

Papers

1. A Study of Prediction and Validation of FEEP Crown needle Internal Porosity for small satellites using CNN(Convolutional Neural Network) and random functions

3. INFLUENCE OF SURFACE AREA AND PROPELLANT MATERIAL ON THE IMPULSE BIT IN ABLATIVE PULSE PLASMA ACELERATOR

4. Sprite-Class Satellites Propulsion to Extended Lifespan

6. Computational Simulation of Neutral Gas Dynamics in the CubeSat Ambipolar Thruster

8. Development and Preliminary Evaluation of Plugim Electrospray Thruster: Focus on the Fuel Management System and Power Processing Unit

9. Experimental Testing and Numerical Simulation Validation of an Air Intake for Air-Breathing Electric Propulsion (ABEP) Systems

10. Fabrication and Testing of Applied Field Magneto Plasma Dynamic Thruster with Argon as Propellant

11. Geometric characteristics optimization and integrated design analysis of Air-Breathing Electric Propulsion inlet

13. optimisation and durability assessment of rf helicon-based plasma thruster (k-2) for very low earth orbit air-breathing electric propulsion

14. stargate: an undergraduate experimental electric propulsion student research project

15. Designing a nuclear electric propulsion system for future Pluto missions

16. Improving rocket nozzle efficiency with rough surfaces

16. Design and structural analysis of low-cost modular rocket engine test stand.

17. Power Sustainment in Long-Duration Space Missions through the Utilization of Nitinol Material Implemented in the Design of Solar Sails, Programmed with PID Control.

19. Advancements in the development of the subsystems for a student-developed H2O2/ABS hybrid propellant rocket engine

20. Innovative Methodology for Evaluating Combustion Efficiency in Swirled Rocket Engines

21. An Improved Al Particle Combustion Model for Simulating the Aluminized Hybrid Rocket Motor Combustion

22. Characterization of Paraffin-LDPE Blended Fuels

23. design of dual-bell nozzle specified for the second stage engine of students' designed sounding rocket

24. Analysis of the nozzle impact on the characteristics of the pulse detonation engine

25. Decomposition mechanism of ammonium dinitramide: a sustainable energetic molecule for green propellant technologies

26. Development and Integration of the Engineering Model for a Modular HTP-based CubeSat Propulsion System for future In-Orbit Validation on the UniPi EXCITE CubeSat Platform

27. Development and Testing of an Electrically-Driven Centrifugal Pressurization System for Hybrid Rockets in Rocket Propulsion

28. Development and validation of rocket motor simulation software

29. Development of Environmentally Friendly Solid Propellants Using Fused Deposition Modeling Additive Manufacturing

30. Development of High-Performance Solid Rocket Propellants Using AP-HTPB Composite Matrix AND Different Plasticizers

32. Dynamic characteristics of hydrogen peroxide electric pump during pulse ignition process of hybrid rocket engine

33. Effect of manufacturing parameters on tungsten microstructures as an emitter for FEEP thrusters

34. Energetic co-crystals containing ammonium nitrate obtained by solvent method as an alternative to solid rocket fuels based on perchlorates

35. Fluidic throat technology for hybrid rocket motor based on liquid oxidizer cooling

37. Introduction of Field Emission Electric Propulsion Research in Republic of Korea

38. INVESTIGATION INTO THE SUITABLE INJECTOR TYPES FOR SMALL-SCALE GASEOUS THRUST CHAMBERS

39. Investigation of Solid Fuel Pyrolysis Characteristics in Hybrid Rocket Engines Utilizing HTPB with Aluminum Additive

40. Low-cost Innovative Experimental Setup for Assessing Laser-Driven Propulsion in Near-Ultimate Vacuum Conditions

41. Maximizing Reusability in Propulsion System Testing: A modular Data Acquisition System Using National Instruments PXI hardware and LabVIEW

42. Numerical Computations of Nozzle Performance Losses in Solid Rocket Motors

43. Numerical Simulation and Experimental Study of the Throat Parallel Segment Length of Variable Area Cavitating Venturi

44. Optimization of pump-valve combined regulation strategy for electric pump-fed system in a hybrid rocket motor

45. Optimizing Launch Systems: Propulsion and Structural Innovations for Enhanced Efficiency in Advanced Vehicles

46. pace hybrid propulsion: a combination of electric and thermonuclear propulsion to optimize satellites

47. Performance testing of small scale resistojet thruster with 3D printed heat exchanger

49. research on mechanism for high nozzle closure opening pressure of solid rocket motor in stage separation

50. Research on cryogenic line chill-down process of industrial Teflon coated piping

51. Research on the performance of the modified paraffin-wax-based fuel grains in the use of Student Researched and Developed (SRAD) hybrid rocket motor

52. research, analysis and experimental development of solid propellant type rnx for rocket engines in environments with humid mountain climate

53. RMD simulations applied to the study of energetic materials like HMX smokeless solid propellant: a case study of HMX molecular vacancies.

54. Systemisation and Performance Testing of Field Emission Electric Propulsion Thruster using Gallium as Propellant

55. development of subcooled liquid oxygen system for liquid rocket engine

57. Thermal Decomposition of Hydrogen Peroxide (H2O2) in the Lab-scale for Space Applications

58. design and cfd analysis of a hypersonic inlet and hydrogen combustion for a scramjet engine at mach 7

59. thermal responsive propellant formulations for variable thrust control for winged space rocket

60. Numerical Design Optimization of a Blow-Down Supersonic Wind Tunnel

62. hybrid propulsion system for spaceplanes: optimizing efficiency and performance

63. Enhancing the Performance of Solid-Fuel Dual Scramjet through Innovative Design and Numerical Investigation

64. Development of an Air-Breathing Electrostatic Thruster

65. Plume characterization of a magnetic nozzle thruster by two-dimensional laser-induced fluorescence measurements

67. Swirl injectors in hybrid rocket engine - design, parameters validation and applicability in a N2O/ABS hybrid rocket booster

68. Conceptual development of modular ion thrusters for its use on nuclear electric propulsion systems.

69. Rapid iterative design of a cost-effective e-pump for a liquid-fuelled reusable sounding rocket: a comprehensive approach to in-house design, manufacturing and testing.

70. SRAD Capacitive Level Sensor for Propellant Measurement of a Liquid Rocket

71. Propulsion systems for Mars mission: alternatives and opportunities

72. Life evaluation of liquid rocket engine regenerative cooling system: a comparison of hardening models

73. Investigation of Hypergolic Ignition of Green Kerosene-based Fuels with HTP

74. Full rotordynamics analysis of a turbopump rotor system

76. Enhancing Reliability in European Rocket Engines: The GTD Approach to Engine Test Bench Control and Monitoring at DLR Lampoldshausen

77. Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters

78. Design of a Propellant Liquefaction and Storage System for Cryogenic Rocket Engine Propellants

80. A novel technique for salvaging a double walled thrust chamber nozzle

81. Experimental Investigation on Pressure and Flow Regulation of Variable Area Cavitation Venturi in Pump-feed System

82. Geometric characteristics optimization and integrated design analysis of Air-Breathing Electric Propulsion inlet

83. Experimental study and modelling of rise time in HAN based monopropellant thruster and its effect on chamber pressure oscillations

84. optical visualization of fuel injector with flat spray nozzle during throttling of H2O2/kerosene bipropellant thruster

85. Closed-Loop Thrust Throttling Capabilities on Kero-Lox Liquid Rocket Engine

86. combustion characteristics of hydroxylammonium nitrate-based electrically controlled gel propellant

87. Regenerative and Liquid Film Cooling: Development of a Unified Thermal Control Strategy in Liquid Rocket Engines

88. Potential of Radial Turbines in Liquid Rocket Engines: a comparative study with classical axial Turbines

89. Dynamic combustion characteristics of the GOX/GCH4 pintle model combustor with different sizes of the mantle recirculation zone

91. Conceptual Design and Fabrication of 400 N-class Multi-hole Pintle GCH4/LOx Injector

92. Characterization and Testing of a 1N Green Monopropellant Micro-Thruster Produced Using Additive Manufacturing Technique

93. Design, Development and Testing of a Five-Thruster Multidirectional Resistojet Propulsion System for cubsats applications

94. Decomposition characteristics of hydrogen peroxide by external heat source in small scale monopropellant thrusters

95. Catalyst-Driven Green Propellant Development for Hypergolic Systems

96. Characterization of Engine Cooldown for a Centrifugal Nuclear Thermal Rocket

98. Optimal trajectories for a spacecraft propelled by an E-sail with piecewise inertially-fixed attitude

99. A Levitated Displacement Interferometer Thrust Stand for Characterization of Propellantless Propulsion Concepts

100. innovations in nuclear and propellantless propulsion technologies

101. molten salt reactor concepts for advanced nuclear electric propulsion (NEP) systems

102. Review of Nuclear Electric Propulsion for Interplanetary Missions

104. Hydrolytic space propulsion: \\ a new opportunity for cubesat missions

105. Optimising Solar Sail Design for Interplanetary Missions: Balancing Mass, Area, and Trajectory

106. THE GREEN FUTURE OF PROPULSION FOR SATELLITES & SPACE VEHICLES

107. The features of LVexisting pressurization systems of propellant tanks and prospects of their development

109. Preliminary study on an electrolysis-based satellite micropropulsor for a 12U cubesat

110. Perspectives on Colloidal Polymeric Nitrogen Monopropellant Engines

111. Optimization study of an upper stage based on an e-pump-fed engine

112. Optimization of thrust control strategy for electric pump-fed rocket engines

113. Modeling, Simulation and Testing of an Innovative Engineering Model Water-based Propulsion Unit for Cubesats

114. Investigation on an efficient thermal pressurization method for propellant tanks of cryogenic upper stage

115. Integrated propulsion control technology for Future Space Transportation Systems

116. In house development of novel, thermally stable ceramic composite catalyst for HAN Decomposition

117. fault simulation study of full-flow staged combustion cycle engine start-up process

118. Dynamics modeling and simulation analysis of reusable high-pressure supplementary combustion liquid oxygen kerosene variable thrust rocket engine: Part I - Single point operating condition analysis

119. Digital Twin Performance Analysis of a 500 pound-thrust, Throttling, Hypergolic Rocket Engine

120. Development of Atlas: A Liquid Rocket Engine Cryogenic Feed System

121. Design, Modeling and Simulations of a High Pressure Cryogenic System for a Space Propulsion Test Facility

122. Design and evaluation of a small scale liquid rocket engine using pineapple’s waste

123. Design and Analysis of a LH2-LOX Rotating Detonation Propulsion System

124. BREAKING BARRIERS WITH BIOFUELS: THE FUTURE OF ROCKET PROPULSION

125. Establishing a Foundation for Rocketry Advancement in Mexico: Development of a Hybrid Rocket Engine.

126. Hybrid Rocket Simulation Using CEQUEL for Thermochemistry Calculations

129. Fundamental Investigation of Micro-Explosive in Aluminum-Lithium Alloy Particle at the Atomic Scale

131. Performance analysis of Paraffin, Beeswax and Magnesium as a fuel for Hybrid Propulsion

132. Experimental investigation of combustion instability inside lab-scale hybrid rocket motor with swirl injector

133. Conceptual design of a 1 kN hybrid rocket engine manufactured with additive technology

134. Numerical modelling approach for the development of an orbital-scale hybrid propulsion engine

135. advancing thermal management: heat flow analysis and hotspot identification in solid rocket motors

136. Thrust Prediction of Hybrid Rocket Motor Based on Physical Feature Embedding and Residual Learning

137. Statistical Thermodynamics Approaches for Advancing Chemical Propulsion Systems

138. Research on charge integrity simulation of brush charge asymmetric ignition of small solid thruster

139. numerical combustion model and efficiency study of electrically ignited solid propellants for micro to macro propulsion systems

140. NUMERICAL AND EXPERIMENTAL ANALYSIS OF NEW PROPELLANT FORMULATIONS FOR HYBRID ROCKETS

142. H2O2/HDPE Hybrid Rocket: Experimental and Theoretical Investigation

143. Development of Carbon Fiber Rocket Motors with Insulative Laminate Structure

144. AI and Classical Approaches to Estimating Solid Fuel Regression Rate in Hybrid Rocket Engines