Satellite Sandwich Structures: Comparison
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Please note this is a comparison between Version 2 by Conner Chen and Version 1 by Riley Carriere.

Sandwich panels are widely used in the design of unmanned satellites and, in addition to having a structural function, can often serve as shielding, protecting the satellites’ equipment from hypervelocity impacts (HVI) of orbital debris and micrometeoroids.

  • orbital debris
  • hypervelocity impact
  • spacecraft shielding
  • sandwich panels
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References

  1. Pelton, J. Space Debris and Other Threats from Outer Space; Springer: Berlin, Germany, 2013.
  2. Christiansen, E. Meteoroid/Debris Shielding; NASA TP-2003-210788; NASA: Houston, TX, USA, 2003.
  3. Protecting the Space Station from Meteoroids and Orbital Debris; National Academies Press: Washington, DC, USA, 1997.
  4. Christiansen, E.; Kornel Nagy, L.; Dana, M.L.; Thomas, G. Space Station MMOD Shielding. Acta Astronaut. 2009, 65, 921–929.
  5. Destefanis, R.; Schäfer, F.; Lambert, M.; Moreno, F.; Schneider, E. Enhanced Space Debris Shields for Manned Spacecraft. Int. J. Impact Eng. 2003, 29, 215–226.
  6. Akahoshi, Y.; Ryuta, N.; Makoto, T. Development of Bumper Shield Using Low Density Materials. Int. J. Impact Eng. 2001, 26, 13–19.
  7. Whipple, F.L. Meteorites and Space Travel. Astronom. J. 1947, 52, 131.
  8. Christiansen, E.L. Design and Performance Equations for Advanced Meteoroid and Debris Shields. Int. J. Impact Eng. 1993, 14, 145–156.
  9. Christiansen, E.; Crews, J.; Williamsen, J.; Robinson, J.; Nolen, A. Enhanced meteoroid and orbital debris shielding. Int. J. Impact Eng. 1995, 17, 217–228.
  10. Destefanis, R.; Faraud, M.; Trucchi, M. Columbus debris shielding experiments and ballistic limit curves. Int. J. Impact Eng. 1999, 23, 181–192.
  11. Arnold, J.; Christiansen, E.L.; Davis, A.; Hyde, J.; Lear, D.; Liou, J.C.; Lyons, F.; Prior, T.; Studor, G.; Ratliff, M.; et al. Handbook for Designing MMOD Protection; NASA JSC-64399, Version A, JSC-17763; NASA: Houston, TX, USA, 2009.
  12. Ryan, S.; Christiansen, E. Micrometeoroid and Orbital Debris (MMOD) Shield Ballistic Limit Analysis Program; NASA/TM–2009–214789; NASA: Houston, TX, USA, 2010.
  13. Protection Manual; IADC-04-03; Inter-Agency Space Debris Coordination Committee, NASA: Houston, TX, USA, 2011.
  14. Adams, D.O.; Webb, N.J.; Yarger, C.B.; Hunter, A.; Oborn, K.D. Multi-Functional Sandwich Composites for Spacecraft Applications: An Initial Assessment; NASA/CR-2007-214880; NASA: Houston, TX, USA, 2007.
  15. Bylander, L.A.; Carlström, O.H.; Christenson, T.S.R.; Olsson, F.G. A Modular Design Concept for Small Satellites. In Smaller Satellites: Bigger Business? Springer: Amsterdam, The Netherlands, 2002; pp. 357–358.
  16. Cherniaev, A.; Telichev, I. Weight-Efficiency of Conventional Shielding Systems in Protecting Unmanned Spacecraft from Orbital Debris. J. Spacecr. Rocket. 2017, 54, 75–89.
  17. Krisko, P.H. The New NASA Orbital Debris Engineering Model ORDEM 30. In Proceedings of the AIAA/AAS Astrodynamics Specialist Conference, San Diego, CA, USA, 4–7 August 2014.
  18. Turner, R.J.; Taylor, E.A.; McDonnell, J.M.; Stokes, H.; Marriott, P.; Wilkinson, J.; Catling, D.J.; Vignjevic, R.; Berthoud, L.; Lambert, M. Cost effective honeycomb and multi-layer insulation debris shields for unmanned spacecraft. Int. J. Impact Eng. 2001, 26, 785–796.
  19. Ryan, S.; Christiansen, E. Hypervelocity Impact Testing of Aluminum Foam Core Sandwich Panels; NASA/TM–2015–218593; NASA: Houston, TX, USA, 2015.
  20. Hyde, J.; Christiansen, E.; Lear, D. Shuttle MMOD Impact Database. Procedia Eng. 2015, 103, 246–253.
  21. Yasensky, J.; Christiansen, E.L. Hypervelocity Impact Evaluation of Metal Foam Core Sandwich Structures; JSC 63945; NASA: Houston, TX, USA, 2007.
  22. Mespoulet, J.; Héreil, P.L.; Abdulhamid, H.; Deconinck, P.; Puillet, C. Experimental study of hypervelocity impacts on space shields above 8 km/s. Procedia Eng. 2017, 204, 508–515.
  23. Lambert, M.; Schäfer, F.K.; Geyer, T. Impact damage on sandwich panels and multi-layer insulation. Int. J. Impact Eng. 2001, 26, 369–380.
  24. Deconinck, P.; Abdulhamid, H.; Héreil, P.L.; Mespoulet, J.; Puillet, C. Experimental and numerical study of submillimeter-sized hypervelocity impacts on honeycomb sandwich structures. Procedia Eng. 2017, 204, 452–459.
  25. Taylor, E.; Herbert, M.; Vaughan, B.; McDonnell, J. Hypervelocity impact on carbon fibre reinforced plastic/aluminium honeycomb: Comparison with whipple bumper shields. Int. J. Impact Eng. 1999, 23, 883–893.
  26. Sibeaud, J.M.; Prieur, C.; Puillet, C. Hypervelocity Impact on Honeycomb Target Structures: Experimental Part. In Proceedings of the 4th European Conference on Space Debris, Darmstadt, Germany, 18–20 April 2005; Volume 587, p. 401.
  27. Taylor, E.; Herbert, M.; Kay, L. Hypervelocity Impact on Carbon Fibre Reinforced Plastic (cfrp)/aluminium Honeycomb at Normal and Oblique Angles. In Proceedings of the Second European Conference on Space Debris, Darmstadt, Germany, 17–19 March 1997; Volume 393, p. 429.
  28. Taylor, E.; Herbert, M.; Gardner, D.J.; Kay, L.; Thomson, R.; Burchell, M.J. Hypervelocity impact on spacecraft carbon fibre reinforced plastic/aluminium honeycomb. Proc. Inst. Mech. Eng. Part G: J. Aerosp. Eng. 1997, 211, 355–363.
  29. Ryan, S.; Schaefer, F.; Riedel, W. Numerical simulation of hypervelocity impact on CFRP/Al HC SP spacecraft structures causing penetration and fragment ejection. Int. J. Impact Eng. 2006, 33, 703–712.
  30. Ryan, S.; Schaefer, F.; Destefanis, R.; Lambert, M. A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures. Adv. Space Res. 2008, 41, 1152–1166.
  31. Schäfer, F.; Destefanis, R.; Ryan, S.; Riedel, W.; Lambert, M. Hypervelocity Impact Testing of CFRP/Al Honeycomb Satellite Structures. In Proceedings of the 4th European Conference on Space Debris, Darmstadt, Germany, 18–20 April 2005; Volume 587, p. 407.
  32. Schaefer, F.K.; Schneider, E.; Lambert, M. Review of Ballistic Limit Equations for Composite Structure Walls of Satellites. In Environmental Testing for Space Programmes; NASA: Houston, TX, USA, 2004; Volume 558, pp. 431–444.
  33. Miller, J.E. Observations of Non-Spherical, Graphite-Epoxy Projectiles Impacting a Thermally-Insulated, Double-Wall Shield. In Proceedings of the 15th Hypervelocity Impact Symposium, Destin, FL, USA, 14–19 April 2019.
  34. Nitta, K.; Higashide, M.; Kitazawa, Y.; Takeba, A.; Katayama, M.; Matsumoto, H. Response of an aluminum honeycomb subjected to hypervelocity impacts. Procedia Eng. 2013, 58, 709–714.
  35. Lambert, M. Hypervelocity impacts and damage laws. Adv. Space Res. 1997, 19, 369–378.
  36. Taylor, E.A.; Glanville, J.P.; Clegg, R.A.; Turner, R.G. Hypervelocity Impact on Spacecraft Honeycomb: Hydrocode Simulation And Damage Laws. Int. J. Impact Eng. 2003, 29, 691–702.
  37. Sibeaud, J.M.; Thamie, L.; Puillet, C. Hypervelocity impact on honeycomb target structures: Experiments and modeling. Int. J. Impact Eng. 2008, 35, 1799–1807.
  38. Liu, P.; Liu, Y.; Zhang, X. Improved shielding structure with double honeycomb cores for hyper-velocity impact. Mech. Res. Commun. 2015, 69, 34–39.
  39. Liu, P.; Liu, Y.; Zhang, X. Simulation of hyper-velocity impact on double honeycomb sandwich panel and its staggered improvement with internal-structure model. Int. J. Mech. Mater. Des. 2016, 12, 241–254.
  40. Giacomuzzo, C.; Pavarin, D.; Francesconi, A.; Lambert, M.; Angrilli, F. SPH evaluation of out-of-plane peak force transmitted during a hypervelocity impact. Int. J. Impact Eng. 2008, 35, 1534–1540.
  41. Nishida, M.; Hayashi, K.; Toya, K. Influence of impact angle on size distribution of fragments in hypervelocity impacts. Int. J. Impact Eng. 2019, 128, 86–93.
  42. Chen, H.; Francesconi, A.; Liu, S.; Lan, S. Effect of honeycomb core under hypervelocity impact: Numerical simulation and engineering model. Procedia Eng. 2017, 204, 83–91.
  43. Miller, J.E. Considerations of Oblique Impacts of Non-spherical, Graphite-epoxy Projectiles. In Proceedings of the 1st International Orbital Debris Conference, Sugarland, TX, USA, 9–12 December 2019.
  44. Cour-Palais, B.G. The shape effect of non-spherical projectiles in hypervelocity impacts. Int. J. Impact Eng. 2001, 26, 129–143.
  45. Christiansen, E.; Crews, J.; Kerr, J.; Cour-Palais, B.; Cykowski, E. Testing the validity of cadmium scaling. Int. J. Impact Eng. 1995, 17, 205–215.
  46. Mullin, S.A.; Littlefield, D.L.; Anderson, C.E., Jr.; Tsai, N.T. Velocity Scaling of Impacts Into Spacecraft Targets at 8 to 15 km/s. In Proceedings of the Hypervelocity Impact Symposium, Austin, TX, USA, 17–20 November 1992.
  47. Schmidt, R.M.; Housen, K.R.; Piekutowski, A.J.; Poormon, K.L. Cadmium simulation of orbital-debris shield performance to scaled velocities of 18 km/s. J. Spacecraft Rockets 1994, 31, 866–877.
  48. Schonberg, W.; Williamsen, J. RCS-based ballistic limit curves for non-spherical projectiles impacting dual-wall spacecraft systems. Int. J. Impact Eng. 2006, 33, 763–770.
  49. Protection Manual; IADC-WD-00-03; Inter Agency Space Debris Coordination Committee, NASA: Houston, TX, USA, 2004.
  50. Frost, C.; Rodriguez, P. AXAF Hypervelocity Impact Test Results. In Proceedings of the Second European Conference on Space Debris, Darmstadt, Germany, 17–19 March 1997; Volume 393, p. 423.
  51. Kang, P.; Youn, S.K.; Lim, J.H. Modification of the critical projectile diameter of honeycomb sandwich panel considering the channeling effect in hypervelocity impact. Aerospace Sci. Technol. 2013, 29, 413–425.
  52. Iliescu, L.E.; Lakis, A.A.; Oulmane, A. Sattelites/Spacecraft Materials and Hypervelocity Impact (HVI) Testing: Numerical Simulations. J. Eng. 2017, 4, 24–64.
  53. Schubert, M.; Perfetto, S.; Dafnis, A.; Mayer, D.; Atzrodt, H.; Schroder, K.U. Multifunctional Load Carrying Lightweight Structures for Space Design; Institute of Structural Mechanics and Lightweight Design; RWTH Aachen University; Fraunhofer Institute for Structural Durability and System Reliability LBF: Darmstadt, Germany, 2017; pp. 1–11.
  54. Ryan, S.J.; Christiansen, E.L.; Lear, D.M. Development of the Next Generation of Meteoroid and Orbital Debris Shields. In AIP Conference Proceedings; American Institute of Physics: College Park, MD, USA, 2009; Volume 1195, pp. 1417–1420.
  55. Pasini, D.L.S.; Price, M.C.; Burchell, M.J.; Cole, M.J. Spacecraft Shielding: An Experimental Comparison Between Open Cell Aluminium Foam Core Sandwich Panel Structures and Whipple Shielding. In Proceedings of the European Planetary Science Congress, London, UK, 8–13 September 2013.
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