Numerical simulation in micrometeoroid and orbital debris risk assessment

Predictive Modeling of Dynamic Processes: A Tribute to Professor Klaus Thoma

Volumn , Issue , 2009, Pages 417-446

  Ryan, Shannon ^a  

^a NASA JOHNSON SPACE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84889980497     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1007/978-1-4419-0727-1_22     Document Type: Chapter

References (27)

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3. Cour-Palais, B.: Hypervelocity Impact Investigations and Meteoroid Shielding Experience Related to Apollo and Skylab. Orbital Debris, 247-275 (1982)
4. Christiansen, E., Kerr, J.: Ballistic Limit Equations for Spacecraft Shielding. International Journal of Impact Engineering 26, 93-104 (2001)
5. Piekutowsi, A.: Fragmentation-Initiation Threshold for Spheres Impacting at Hypervelocity. International Journal of Impact Engineering 29, 563-574 (2003)
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7. Christiansen, E.: Meteoroid/Debris Shielding. NASA Johnson Space Center, Houston, NASA TP-2003-120788 (2003)
8. McMillan A.: Experimental Investigations of SimulatedMeteoroid Damage to Various Spacecraft Structures, General Motors Corporation, Santa Barbara, NASA CR-915 (1968)
9. Schonberg, W., Copper, D.: Repeatability and Uncertainty Analyses of NASA/MSFC Light Gas Gun Test Data. University of Alabama, Huntsville, NASA CR-192496 (1993)
10. Christiansen, E., Crews, J., Williamsen, J., Robinson, J., Nolen, A.: Enhanced Meteoroid and Orbital Debris Shielding 17, 217-228 (1995)
11. Frost, V.: Meteoroid Damage Assessment-NASA Space Vehicle Design Criteria (Structures). Aerospace Corporation, Langley, NASA SP-8042 (1970)
12. Schmidt, R., Housen, K.: Cadmium Simulation of Orbital-Debris Shield Performance to Scaled Velocities of 18 km/s. Journal of Spacecraft and Rockets 31(5), 866-877 (1994)
13. Christiansen, E., Crews, J., Kerr, J., Cour-Palais, B., Cykowski, E.: Testing the Validity of Cadmium Scaling. International Journal of Impact Engineering 17, 205-215 (1995)
14. Palmieri, D., Faraud, M., Destefanis, R., Marchetti, M.: Whipple Shield Ballistic Limit at Impact Velocities Higher Than 7 km/s. Int. J. of Impact Engineering 26, 579-590 (2001)
15. Kerr, J., Fahrenthold, E.: Three Dimensional Hypervelocity Impact Simulation for Orbital Debris Shield Design. International Journal of Impact Engineering 20, 479-489 (1997)
16. Schaefer, F., Ryan, S., Destefanis, R., Rott, M., Mandeville, J.: Composite Materials Impact Damage Analysis-Final Report. FhG EMI, Freiburg, Report No. I-69/05 (2005)
17. Riedel, W., Nahme, H., White, D., Clegg, R.: Advanced Material Model for Hypervelocity Impact Simulations (ADAMMO), FhG EMI, Freiburg, ESA CR(P) 4397 (2003)
18. Anon.: ANSYS AUTODYN User Manual-Version 11.0, Century Dynamics Inc., Concord (2007)
19. Ryan, S., Riedel, W., Schaefer, F.: Numerical Study of Hypervelocity Space Debris Impacts on CFRP/Al Honeycomb Spacecraft Structures. 55th IAC, Vancouver (2004)
20. Ryan, S., Schaefer, F., Lambert, M.: A Ballistic Limit Equation for Hypervelocity Impacts on CFRP/Al HC Satellite Structures 41, 1152-1166 (2008)
21. Putzar, R., Schaefer, F., Romberg, O., Stokes, H., Heine, A., Zimmermann, J.: Vulnerability of Spacecraft Equipment to Space Debris and Meteoroid Impacts-Final Report. Fraunhofer Ernst-Mach-Institut (EMI), Freiburg, Report No. I-15/06 (2006)
22. Ryan, S., Riedel, W.: Preliminary Theoretical Material Characterization for Numerical Modelling of Composite Structures. 56th IAC, Fukuoka, IAC-05-C2.5.10 (2005)
23. Ryan, S., Schaefer, F., Riedel, W.: Numerical Simulation of Hypervelocity Impact on CFRP/Al HC SP Spacecraft Structures Causing Penetration and Fragment Ejection. International Journal of Impact Engineering 33(1-2), 703-712 (2006)
24. Ryan, S.,Wicklein, M., Mouritz, A., Riedel,W., Schaefer, F., Thoma, K.: Theoretical Prediction of Dynamic Composite Material Properties for Hypervelocity Impact Simulations. Int. Journal of Impact Engineering (2009)
25. Ryan, S., Schaefer, F., Guyot, M., Hiermaier, S., Lambert, M.: Characterizing the Transient Reponse of CFRP/Al HC Spacecraft Structures Induced by Space Debris Impact at Hypervelocity. International Journal of Impact Engineering 35, 1756-1763 (2008)
26. Ryan, S.: Hypervelocity Impact Induced Disturbances on Composite Sandwich Panel Spacecraft Structures. Forschungsergebnisse aus der Kurzzeitdynamik-No. 15, Fraunhofer Institut fuer Kurzzeitdynamik, Freiburg, ISBN 978-3-8167-7522-5 (2008)
27. Vergniaud, J., Guyot,M., Lambert, M., Schaefer, F., Ryan, S., Hiermaier, S., Taylor, E.: Structural Vibrations Induced by HVI-Application to the GAIA Spacecraft. International Journal of Impact Engineering 35, 1836-1843 (2008)