Schäfer, F.F.SchäferDestefanis, R.R.DestefanisRyan, S.S.RyanRiedel, W.W.RiedelLambert, M.M.Lambert2022-03-102022-03-102005https://publica.fraunhofer.de/handle/publica/348270en620Hypervelocity impact testing of CFRP/Al Honeycomb satellite structuresconference paper