All Stories

  1. Rapid prototyping of satellite shields: 3D printed carbon fiber and Kevlar composites for hypervelocity impact protection
  2. ASTROBEAT: Advancing cold-welding technology for in-situ spacecraft repairs
  3. Simulation and validation of a fragmentation model for carbon fibre reinforced polymers subjected to hypervelocity collision
  4. A novel size distribution model for debris generated by in-orbit collisions
  5. The J2050 student PocketQube for space debris investigation and optical observation technology development
  6. Autonomous Docking Manoeuvre Testing in the Framework of the ERMES Experiment
  7. Hypervelocity impact against aluminium Whipple shields in the shatter regime with systematic parameter variation: An experimental and numerical study
  8. SPRISS: Scalable and precise resistive impact sensor for smallsats, architecture description and tests
  9. Hypervelocity Impact Testing and Simulation at the University of Padova
  10. Ballistic Limit Equation Derivation for Thin Tape Tethers
  11. Development and Preliminary Testing of the ATEMO Multi-Purpose Sensing Platform
  12. Investigation of aluminium Whipple Shield response to hypervelocity impacts close to ballistic limit between 2.5 and 5 km/s
  13. Overview of Spacecraft-Fragmentation Testing
  14. Concept and Feasibility Analysis of the Alba Cubesat Mission
  15. Numerical simulation of COSMOS 2499 fragmentation
  16. Editorial for Special Issue: Recent Advances in Space Debris
  17. A New Charateristich Length Debris Distribution Model for In-Space Collision Events
  18. A Numerical Model for CFRP Fragmentation Under Hypervelocity Impacts
  19. Analysis of delta-V Distributions of In-Space Fragmentation Events
  20. Earth Observation with Autonomous Systems on Board Sounding Balloons
  21. Ground-Based Experimental Reflectance Verification for Satellite Hypervelocity Impact Characterization
  22. Numerical Implementation of Empirical Distribution Models for Spacecraft Fragmentation
  23. Rupture Models for Tanks for Space Applications
  24. Supporting the Italian Space Surveillance and Tracking Research Activities
  25. Simulation of In-Space Fragmentation Events
  26. Ascent trajectory of sounding balloons: dynamical models and mission data reconstruction
  27. Concept and feasibility analysis of the Alba CubeSat mission
  28. Development of a smart docking system for small satellites
  29. Exploring aerospace advancements and global collaborations: a comprehensive analysis of MCAST's aerospace program in Malta
  30. Feasibility analysis of a CubeSat mission for space rider observation and docking
  31. Mechanical and pneumatic design and testing of a floating module for zero-gravity motion simulation
  32. Overview of spacecraft fragmentation testing
  33. Simulation of in-space fragmentation events
  34. The ATEMO device: a compact solution for earth monitoring
  35. Cold welding adhesion for spacecraft repair: Experiment design and roadmap
  36. Kinematic tests on a docking mechanism for microsatellites
  37. Analysis of Fragment Distributions from Carbon-Fiber-Reinforced Composite Panels Subjected to Hypervelocity Impacts
  38. Simulations of satellites mock-up fragmentation
  39. Research at the University of Padova in the Field of Space Debris Impacts against Satellites: An Overview of Activities in the Last 10 Years
  40. Analysis of fragments larger than 2 mm generated by a picosatellite fragmentation experiment
  41. Laser Vibrometry-Based Precise Measurement of Tape-Shaped Tethers Damping Ratio Toward Space Applications
  42. Mechanisms for CubeSats and SmallSats
  43. Preliminary observation of Marmolada glacier collapse of July 2022 with space-based cameras
  44. Experimental fragments distributions for thin aluminium plates subjected to hypervelocity impacts
  45. Launch of a sounding balloon for horizontal and vertical modelling of ALAN propagation in the atmosphere
  46. Characterization of the fragments generated by a Picosatellite impact experiment
  47. Validation of enabling technologies for deorbiting devices based on electrodynamic tethers
  48. Assessment of optical surfaces deterioration due to dust and ice impact and deposition
  49. Measurement of mechanical characteristics of tape tethers for space applications
  50. Deorbit kit demonstration mission
  51. Numerical simulations of hypervelocity collisions scenarios against a large satellite
  52. ERMES: Design and preliminary simulations for an autonomous docking manoeuvre
  53. Evaluation of a Single-Stage Light-Gas Gun Facility in Malta: Business Analysis and Preliminary Design
  54. Flight test of an autonomous payload for measuring sky brightness and ground light pollution using a stratospheric sounding balloon
  55. An in-line damper for tethers-in-space oscillations dissipation
  56. Verification of Angular Response of Sky Quality Meter with Quasi-Punctual Light Sources
  57. Impact risk assessment of deorbiting strategies in Low Earth Orbits
  58. A conceptual study to characterize properties of space debris from hypervelocity impacts through Thin Film Heat Flux Gauges
  59. Design and testing of an autonomous ARTVA detector for small drones
  60. Experimental Validation of a Deployment Mechanism for Tape-tethered Satellites
  61. Monitoring of air pollutants using a stratospheric balloon
  62. Space tethers: parameters reconstructions and tests
  63. Deployment requirements for deorbiting electrodynamic tether technology
  64. Test of Tethered Deorbiting of Space Debris
  65. Miniature docking mechanism for CubeSats
  66. Avalanche Rescue with Autonomous Drones
  67. Experimental characterization of multi-layer 3D-printed shields for microsatellites
  68. Large constellations assessment and optimization in LEO space debris environment
  69. CST: A new semi-empirical tool for simulating spacecraft collisions in orbit
  70. TED Project: Conjugating Technology Development and Educational Activities
  71. Development of a low-cost sun sensor for nanosatellites
  72. Study of dynamical stability of tethered systems during space tug maneuvers
  73. Autoport Project: a Docking Station for Planetary Exploration Drones
  74. Design and test of a semiandrogynous docking mechanism for small satellites
  75. Low-cost relative navigation sensors for miniature spacecraft and drones
  76. ARCADE-R2 experiment on board BEXUS 17 stratospheric balloon