1. Anon. Effectiveness of Aluminum Honeycomb Shields in Preventing Meteoroid Damage to Liquid-Filled Spacecraft Tanks, NASA CR-65261, Johnson Space Center, Houston, Texas, 1964.
2. Application of wavelet transform to analyze acceleration signals generated by HVI on thin aluminum plates and all-aluminum honeycomb sandwich panels;Bettella;Int. J. Impact Eng.,2008
3. Blosser, M.L. Development of metallic thermal protection systems for the reusable launch vehicle, in: El-Genk, M.S. (Ed.), Proceedings of the Space Technology and Applications International Forum, AIP CP 387, American Institute of Physics, Woodbury, New York, pp. 1125–1144, 1997.
4. Hypervelocity impact simulation using membrane particle elements;Bohannan;Int. J. Impact Eng.,2008
5. Hypervelocity testing of advanced shielding concepts for spacecraft against impacts to 10km/s;Boslough;Int. J. Impact Eng.,1993