Abstract
Spacecraft that are launched to operate in Earth orbit are susceptible to impacts by meteoroids and pieces of orbital debris (MOD). The effect of a MOD particle impact on a spacecraft depends on where the impact occurs, the size, composition, and speed of the impacting object, the function of the impacted system. In order to perform a risk analysis for a particular spacecraft under a specific mission profile, it is important to know whether or not the impacting particle (or its remnants) will exit the rear of an impacted spacecraft wall. A variety of different ballistic limit equations (BLEs) have been developed for many different types of structural wall configurations. BLEs can be used to optimize the design of spacecraft wall parameters so that the resulting configuration is able to withstand the anticipated variety of on-orbit high-speed impact scenarios. While the level of effort exerted in studying the response of metallic multi-wall systems to high speed particle impact is quite substantial, the extent of the effort to study composite material and composite structural systems under similar impact conditions has been much more limited. This paper presents an overview of the activities performed to assess the resiliency of composite structures and materials under high speed projectile impact. The activities reviewed will be those that have been aimed at increasing the level of protection afforded to spacecraft operating in the MOD environment, and more specifically, on those activities performed to mitigate the mechanical and structural effects of an MOD impact.
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References
Schonberg WP (2001). Protecting Spacecraft Against Meteoroid/Orbital Debris Impact Damage: An Overview. Space Debris, 1:195-210.
Schonberg WP (2008). The Development of Ballistic Limit Equations for Dual-Wall Spacecraft Shielding: A Concise History and Suggestions for Future Development, Proceedings of the 49th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, AIAA Paper No. 2008-1966, Chicago, IL.
Williams JG, Goodman GP (1965). Structural and Materials Investigation of a 1/8-Scale-Model Space Structure of Toroidal Configuration and Filamentary Construction. NASA TN-D-2652, Washington, DC.
McMillan AR (1966). Hypervelocity Impacts into Stainless-Steel Tubes Armored with Reinforced Beryllium. NASA TN-D-3512, Washington, DC.
Cour-Palais BG (1969). Meteoroid Protection by Multiwall Structures. Proceedings of the 1969 Hypervelocity Impact Conference, Cincinnati, Ohio.
Williams JG (1971). High-Velocity-Impact Tests Conducted with Polyethylene Terephthalate Projectiles and Flexible Composite Wall Panels. NASA TN-D-6135, Washington, DC.
Cour-Palais BG (1987). Hypervelocity Impact in Metals, Glass and Composites. International Journal of Impact Engineering, 5:221-237.
Yew CH, Kendrick RB (1987). A Study of Damage in Composite Panels Produced by Hypervelocity Impact. International Journal of Impact Engineering, 5:729-738.
Christiansen EL (1987). Evaluation of Space Station Meteoroid/Debris Shielding Materials. Report No. 87-163, Eagle Engineering Inc, Texas.
Tennyson RC, Shortliffe GD (1997). Hypervelocity Impact Tests on Composite Boom Structures for Space Robot Applications. Canadian Aeronautics and Space Journal, 43(3), 195-202.
Tennyson RC, Shortliffe GD (1997). MOD Impact Damage on Composite Materials in Space. Proceedings of the 7th International Symposium on Materials in a Space Environment, Toulouse, France, p. 485-492. ESA SP, Noordwijk, Netherlands.
Salome R, et al (2001). High Pressure Composite Tank Behavior under a Hypervelocity Impact. In: Proceedings of the Third European Conference on Space Debris, H. Sawaya-Lacoste, ed. ESA SP-473, 2:621-627, Noordwijk, Netherlands.
Finckenor M (1992). Meteoroid/Space Debris Impacts on MSFC LDEF Experiments. LDEF: 69 Months in Space. First Post-Retrieval Symposium, Part 1, 435-442. NASA Langley Research Center.
Tennyson RC (1992). Additional Results on Space Environmental Effects on Polymer Matrix Composites: Experiment A0180. LDEF Materials Workshop 1991, Part 2, 571-592, NASA Langley Research Center.
Tennyson RC, et al (1992). Proposed Test Program and Data Base for LDEF Polymer Matrix Composites. LDEF Materials Workshop 1991, Part 2, 593-600, NASA Langley Research Center.
Roybal R (1995). A New Technique for Ground Simulation of Hypervelocity Debris , LDEF: 69 Months in Space. Third Post-Retrieval Symposium, Part 3, 1379-1388, NASA Langley Research Center.
Lamontange C, et al (1999). Normal and Oblique Hypervelocity Impacts on Carbon Fiber/Peek Composites. International Journal of Impact Engineering, 23:519-532.
Tennyson RC, Lamontange C (2000). Hypervelocity Impact Damage to Composites. Composites Part A, 31:785-794.
Tennyson RC, Lamontange C (2000). High-Velocity Impact Damage to Polymer Matrix Composites. In: Impact Behavior of Fiber-Reinforced Composite Materials and Structures, S. R. Reid and G. Zhou, eds., 280-299, Woodhead Publishing Ltd., England.
Lamontange C, Manuelpillai GN, et al (2001). Projectile Density, Impact Angle and Energy Effects on Hypervelocity Impact Damage to Carbon Fiber/Peek Composites. International Journal of Impact Engineering, 26:381-398.
Daigo K, et al (2004). Hypervelocity Impact Studies on Composite Material. Paper No. IAC-04-IAA.5.12P.03, Proceedings of the 55th Congress of the International Astronautical Federation, Vancouver, Canada.
Unda J, et al (1994). Residual Strength of CFRP Tubes Subjected to Hypervelocity Debris Impact. Paper No. IAF-94-I.5.212, Proceedings of the 45th Congress of the International Astronautical Federation, Jerusalem, Israel.
Verker R, et al (2007). Residual Stress Effect on Degradation of Polyimide under Simulated Hypervelocity Space Debris and Atomic Oxygen. Polymer, 48:19-24.
Sil’vestrov VV, et al (1995). Hypervelocity Impact on Laminate Composite Panels. International Journal of Impact Engineering, 17:751-762.
Homae T, et al (2006). Hypervelocity Planar Plate Impact Experiments of Aramid Fiber-reinforced Plastics. Journal of Reinforced Plastics and Composites, 25(11):1215-1221.
Clegg RA, White DM, et al (2006). Hypervelocity Impact Damage Prediction in Composites. Part I - Material Model and Characterization. International Journal of Impact Engineering, 33:190-200.
Riedel W, Nahme H, et al (2006). Hypervelocity Impact Damage Prediction in Composites. Part II - Experimental Investigations and Simulations. International Journal of Impact Engineering, 33:670-680.
Cheng WL, Langlie S, et al (2003). Hypervelocity Impact of Thick Composites. International Journal of Impact Engineering, 29:167-184.
Lee M (2003). Hypervelocity Impact into Oblique Ceramic/Metal Composite Systems. International Journal of Impact Engineering, 29:417-424.
Munjal AK, et al (1990). Impact Damage Evaluation of Graphite/Epoxy Composite Materials for Space Applications. Proceedings of the 22nd International SAMPE Technical Conference, 1200-1207, Boston, Massachusetts.
Tennyson RC, Manuelpillai G (1994). Prediction of Space Hypervelocity Impact Damage in Composite Materials. Proceedings of the 8th CASI Conference on Astronautics, Ottawa, Canada, 441-450.
White DM, Taylor EA, et al (2003). Numerical Simulation and Experimental Characterization of Direct Hypervelocity Impact on a Spacecraft Hybrid Carbon Fiber/Kevlar Composite Structure. International Journal of Impact Engineering, 29:779–790.
Grujicic M, et al. (2006). Hypervelocity Impact Resistance of Reinforced Carbon–Carbon/Carbon–Foam Thermal Protection Systems. Applied Surface Science, 252:5035–5050.
Schonberg WP (1990). Hypervelocity Impact Response of Spaced Composite Material Structures, International Journal of Impact Engineering, 10:509-523.
Li Y, et al (2004). Energy-Absorption Performance of Porous Materials in Sandwich Composites under Hypervelocity Impact Loading. Composite Structures, 64:71–78.
Colombo P, et al (2003). Effect of Hypervelocity Impact on Microcellular Ceramic Foams from a Preceramic Polymer. Advanced Engineering Materials, 5(11):802-805.
Robinson JH, Nolen AM (1995). An Investigation of Metal Matrix Composites as Shields for Hypervelocity Orbital Debris Impacts. International Journal of Impact Engineering, 17: 685-696.
Sil’vestrov VV, et al (1999). Protective Properties of Shields of Ceramic/Aluminum Composite for Hypervelocity Impact. Combustion, Explosion, and Shock Waves, 35(3):7.
Sil’vestrov VV, Plastinin AN, et al (1999). An Investigation of Ceramic/Aluminum Composites as Shields for Hypervelocity Impacts. International Journal of Impact Engineering, 23:859-867.
Tamura H, Mutou Y (2005). Quantitative Analysis of Debris Clouds from SiC-Fiber-Reinforced Silicon Nitride Bumpers. International Journal of Impact Engineering, 31:1192-1207.
Schonberg WP, Walker EJ (1991). Use of Composite Materials in Multi-Wall Structures to Prevent Perforation by Hypervelocity Projectiles. Composite Structures, 19:15-40.
Katz S, et al (2008). Response of Composite Materials to Hypervelocity Impact. International Journal of Impact Engineering, 35:1606-1611.
Cour-Palais BG, Crews JL (1990) A Multi-Shock Concept for Spacecraft Shielding. International Journal of Impact Engineering, 10:135-146.
Boslough MB, Chhabildas LC, et al (1993). Hypervelocity Testing of Advanced Shielding Concepts for Spacecraft Against Impacts to 10 km/s. International Journal of Impact Engineering, 1993, 14:95-106.
Cour-Palais BG, Piekutowski AJ, et al (1993). Analysis of the UDRI Tests on Nextel Multi-Shock Shields. International Journal of Impact Engineering, 14:193-204.
Thompson LE, Johnson MS (1993). Response of Woven Ceramic Bumpers to Hypervelocity Impacts. International Journal of Impact Engineering, 14:739-749.
Christiansen EL, Kerr JH (1993). Mesh Double-Bumper Shield: A Low-Weight Alternative for Spacecraft Meteoroid and Orbital Debris Protection. International Journal of Impact Engineering, 14:169-180.
Horz F, Cintala MJ (1993). Impact Experiments into Multiple-Mesh Targets: Concept Development of a Lightweight Collisional Bumper, NASA-TM-104764, Johnson Space Center, Houston, Texas.
Christiansen EL. (1993). Design and Performance Equations for Advanced Meteoroid and Debris Shields. International Journal of Impact Engineering, 14:145-156.
Lambert M, Schneider E (1995). Shielding Against Space Debris. A Comparison Between Different Shields: The Effect of Materials on their Performances. International Journal of Impact Engineering, 17:477-485.
Horz F, Cintala MJ, et al (1995) Multiple-Mesh Bumpers: A Feasibility Study. International Journal of Impact Engineering, 17:431-442.
Christiansen EL, Crews JL, et al (1995). Enhanced Meteoroid and Orbital Debris Shielding. International Journal of Impact Engineering, 17:217-228.
Destefanis R, Faraud M (1997). Testing of Advanced Materials for High Resistance Debris Shielding. International Journal of Impact Engineering, 20:209-222.
Munjal AK (1998). Minimizing Hypervelocity Micrometeoroid Impact Damage to Composite Space Structures. Paper No. III.4, Proceedings of the 1998 Leonid Meteoroid Storm and Satellite Threat Conference, The Aerospace Corporation, Los Angeles, California.
Christiansen EL, Kerr JH (1997). Projectile Shape Effects on Shielding Performance at 7 km/s and 11 km/s. International Journal of Impact Engineering, 20:165-172.
Schonberg WP, Williamsen JE (1997). Empirical Hole Size and Crack Length Models for Dual-Wall Systems Under Hypervelocity Projectile Impact. International Journal of Impact Engineering, 20:711-722.
Schonberg WP, Williamsen JE (1999). Modeling Damage in Spacecraft Impacted by Orbital Debris Particles. Journal of Astronautical Sciences, 47:103-115.
Williamsen JE, Evans HA, Schonberg WP (1999). Effect of Multi-Wall System Composition on Survivability for Spacecraft Impacted by Orbital Debris. Space Debris, 1(1):37–43.
Schonberg WP, Walker EJ (1994). Hypervelocity Impact of Dual-Wall Structures with Graphite/Epoxy Inner Walls. Composites Engineering, 4(10):1045-1054.
Ito R, Sekine H (2006). Ballistic Limits of GR/EP and Hybrid Composite Rear Walls Protected by a Debris Shield. International Journal of the Society of Materials Engineering for Resources, 13(2):118-122.
Anon (1964). Effectiveness of Aluminum Honeycomb Shields in Preventing Meteoroid Damage to Liquid-Filled Spacecraft Tanks, NASA CR-65261, Johnson Space Center, Houston, Texas.
Sennett RE, Lathrop BL (1968). The Effects of Hypervelocity Impact on Honeycomb Structures. Paper No. 68-314, Proceedings of the 9th AIAA Structures, Structural Dynamics, and Materials Conference, Palm Springs, California.
Jex DW, Miller AM, McKay CA (1970). The Characteristics of Penetration for a Double-Sheet Structure with Honeycomb, NASA TM-X-53974, Marshall Space Flight Center, Huntsville, Alabama.
Terrillon F, Warren HR, Yelle MJ (1991). Orbital Debris Shielding Design of the RadarSat Spacecraft. Paper No. IAF-91-283, Proceedings of the 42nd International Astronautical Congress, Canada.
Frost CL, Rodriguez PI (1997). AXAF Hypervelocity Impact Test Results Proceedings of the 2nd European Conference on Space Debris, W. Flury, ed., ESA SP-393, 423-428, Noordwijk, The Netherlands.
Sanchez GA, Kerr JH (1996). Advanced X-Ray Astrophysics (AXAF) Meteoroid and Orbital Debris (M/OD) Test Report, Report No. JSC-27354, Johnson Space Center, Houston, Texas.
Shephard GLY, Scheer SA (1993). Secondary Debris Impact Damage and Environment Study. International Journal of Impact Engineering, 14:671-682.
Frate DT, Nahra HK (1996). Hypervelocity Impact Testing of Nickel-Hydrogen Battery Cells. AIAA Paper No. 96-4292, Proceedings of the 1996 AIAA Space Programs and Technologies Conference, Huntsville, Alabama (also NASA TM-107325).
Blosser ML (1997). Development of Metallic Thermal Protection Systems for the Reusable Launch Vehicle. Proceedings of the Space Technology and Applications International Forum, Albuquerque, New Mexico.
Taylor EA, et al (1997). Hypervelocity Impact on Spacecraft Carbon Fiber Reinforced Plastic / Aluminum Honeycomb. Proceedings of the Institution of Mechanical Engineers (UK), 211(G):355-363.
Taylor EA, Herbert MK, Kay L (1997). Hypervelocity Impact on Carbon Fiber Reinforced Plastic (CFRP) / Aluminum Honeycomb at Normal and Oblique Angles. Proceedings of the 2nd European Conference on Space Debris, W. Flury, ed., ESA SP-393, 429-434, Noordwijk, The Netherlands.
Herbert MK, Taylor EA (1998). Hypervelocity Impact Response of Honeycomb: Shielding Performance and Spacecraft Subsystem Design Issues. Proceedings of the Hypervelocity Impact Shielding Workshop, H. Fair, ed., Institute for Advanced Technologies, Austin, Texas.
Taylor EA (1998). Cost Effective Debris Shields for Unmanned Spacecraft. Proceedings of the Hypervelocity Impact Shielding Workshop, H. Fair, ed., Institute for Advanced Technologies, Austin, Texas.
Taylor EA, et al (1999). Hypervelocity Impact on Carbon Fiber Reinforced Plastic / Aluminum Honeycomb: Comparison with Whipple Bumper Shields. International Journal of Impact Engineering, 23:863-893.
Schäfer F (1999). Impact Tests on Metop Sandwich Panels with MLI, EMI Report E-05/99, Ernst Mach Institute, Freiburg, Germany.
Turner RG, Taylor EA (2000). Cost Effective Debris Shields For Unmanned Spacecraft, Final Report, ESA Contract No. 12378/97/NL, Matra Marconi Space.
Turner RG, Taylor EA, et al (2001). Cost Effective Debris Shields for Unmanned Spacecraft. International Journal of Impact Engineering, 26:785-796.
Taylor EA, et al (2003). Hypervelocity Impact on Spacecraft Honeycomb; Hydrocode Simulation and Damage Laws. International Journal of Impact Engineering, 29:691-702.
Sibeaud JM, Prieur C, Puillet C (2005). Hypervelocity Impact on Honeycomb Target Structures. Proceedings of the 4th European Conference on Space Debris, W. Flury, ed., ESA SP-587, Noordwijk, The Netherlands.
Sibeaud JM, Thamie L, Puillet C (2008). Hypervelocity Impact on Honeycomb Target Structures: Experiments and Modeling International Journal of Impact Engineering, 35(12):1799-1807.
Schäfer F, Schneider E (1996). Hypervelocity Impacts on CFRP, EMI Report CFRP-01, Ernst Mach Institute, Freiburg, Germany.
Lambert M (1997). Hypervelocity Impacts and Damage Laws. Advances in Space Research, 19(2):369-378.
Schäfer F (1999). Impact Tests on Rosetta Sandwich Panels with MLI, EMI Report E-02/99, Ernst Mach Institute, Freiburg, Germany.
Schäfer F (1999). Impact Tests on ATV Sandwich Panels, EMI Report E-11/99, Ernst Mach Institute, Freiburg, Germany.
Lambert M, Schäfer F, Geyer T (2001). Impact Damage on Sandwich Panels and Multi-Layer Insulation. International Journal of Impact Engineering, 21:369-380.
Ryan S, Riedel W, Schäfer F (2004). Numerical Study of Hypervelocity Space Debris Impacts on CFRP/Al Honeycomb Spacecraft Structures. Paper No. IAC-04-W.1.02, Proceedings of the 55th International Astronautical Congress, Vancouver, Canada.
Schäfer F, Schneider E, Lambert M (2004). Review of Ballistic Limit Equations for CFRP Structure Walls of Satellites. Proceedings of the 5th International Symposium on Environmental Testing for Space Programs, ESA SP-558, Noordwijk, The Netherlands.
Schäfer F, et al (2005). Hypervelocity Impact Testing of CFRP/AL Honeycomb Satellite Structures. Proceedings of the 4th European Conference on Space Debris, W. Flury, ed., ESA SP-587.
Schäfer F (2005). Composite Materials Impact Damage Analysis, EMI Report I-83-05, Ernst Mach Institute, Freiburg, Germany.
Ryan S, Schäfer F, Riedel W (2006). Numerical Simulation of Hypervelocity Impact on CFRP/Al HC/SP Spacecraft Structures Causing Penetration and Fragment Ejection. International Journal of Impact Engineering, 33:703-712.
Wicklein M (2006). Carbon Fiber Material Models for Hypervelocity Impact Simulations: Testing, EMI Report No. I-73/06, Ernst Mach Institute, Freiburg, Germany.
Putzar R, Schäfer F, et al (2005). Vulnerability of Shielded Fuel Pipes and Heat Pipes to Hypervelocity Impacts. Proceedings of the 4th European Conference on Space Debris, W. Flury, ed., ESA SP-587, Noordwijk, The Netherlands.
Putzar R, Schäfer F, et al (2005). Vulnerability of Spacecraft Electronic Boxes to Hypervelocity Impacts. Paper No. IAC-05-B.6.4.02, Proceedings of the 56th International Astronautical Congress, Fukuoka, Japan.
Schäfer F, Putzar R (2006). Vulnerability of Spacecraft Equipment to Space Debris and Meteoroid Impacts, EMI Report I-15-06, Ernst Mach Institute, Freiburg, Germany.
Schäfer F, Ryan S, et al (2008). Ballistic Limit Equation for Equipment Placed Behind Satellite Structure Walls. International Journal of Impact Engineering, 35:1784-1791.
Ryan S, Schäfer F, et al (2007). A Ballistic Limit Equation for Hypervelocity Impacts on Composite Honeycomb Sandwich Panel Satellite Structures. Advances in Space Research, 41(7):1152-1166.
Schonberg WP, Schäfer F, Putzar R (2009). Effectiveness of HC/SP Ballistic Limit Equations in Predicting Perforation / Non-Perforation Response. Journal of Spacecraft and Rockets, submitted for publication consideration.
Ryan, S (2009). Numerical Simulation in Micrometeoroid and Orbital Debris Risk Assessment. In Predictive Modeling of Dynamic Processes: A Tribute to Klaus Thoma, ed. S. Hiermaier, Springer, Berlin Germany.
Schonberg WP, Schäfer F, Putzar R (2009). Hypervelocity Impact Response of Honeycomb Sandwich Panels, Acta Astronautica, submitted for publication consideration.
Acknowledgments
The author is grateful for the support provided by the Humboldt Foundation through a Fraunhofer-Bessel Research Award that enabled some of the studies whose results were discussed in this paper.
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Schonberg, W.P. (2009). Assessing the Resiliency of Composite Structural Systems and Materials Used in Earth-Orbiting Spacecraft to Hypervelocity Projectile Impact. In: Hiermaier, S. (eds) Predictive Modeling of Dynamic Processes. Springer, Boston, MA. https://doi.org/10.1007/978-1-4419-0727-1_21
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