Influence of space debris impact on solar array under power generation Y Akahoshi, T Nakamura, S Fukushige, N Furusawa, S Kusunoki, ... International Journal of Impact Engineering 35 (12), 1678-1682, 2008 | 62 | 2008 |
Preliminary study on sustained arc due to plasma excited by hypervelocity impact of space debris on the solar array coupon T Harano, Y Machida, S Fukushige, T Koura, S Hosoda, M Cho, ... International Journal of Impact Engineering 33 (1-12), 326-334, 2006 | 57 | 2006 |
Comparison of debris environment models; ORDEM2000, MASTER2001 and MASTER2005 S Fukushige, Y Akahoshi, Y Kitazawa, T Goka IHI engineering review 40 (1), 31, 2007 | 53 | 2007 |
Small carry-on impactor of Hayabusa2 mission T Saiki, H Sawada, C Okamoto, H Yano, Y Takagi, Y Akahoshi, ... Acta Astronautica 84, 227-236, 2013 | 49 | 2013 |
Hypervelocity impact tests against metallic meshes M Higashide, M Tanaka, Y Akahoshi, S Harada, F Tohyama International Journal of Impact Engineering 33 (1-12), 335-342, 2006 | 48 | 2006 |
Solar-array arcing due to plasma created by space-debris impact S Fukushige, Y Akahoshi, K Watanabe, T Nagasaki, K Sugawara, T Koura, ... IEEE Transactions on plasma science 36 (5), 2434-2439, 2008 | 41 | 2008 |
Evolution of ISO's space debris mitigation standards H Stokes, Y Akahoshi, C Bonnal, R Destefanis, Y Gu, A Kato, ... Journal of Space Safety Engineering 7 (3), 325-331, 2020 | 33 | 2020 |
Molecular dynamics simulation on fracture mechanisms of nano-scale polycrystal under static and cyclic loading H INOUE, Y Akahoshi, S HARADA Journal of the Society of Materials Science, Japan 44 (501Appendix), 95-99, 1995 | 28 | 1995 |
Development of a lightweight space debris shield using high strength fibers M Tanaka, Y Moritaka, Y Akahoshi, R Nakamura, A Yamori, S Sasaki International journal of impact engineering 26 (1-10), 761-772, 2001 | 25 | 2001 |
Development of bumper shield using low density materials Y Akahoshi, R Nakamura, M Tanaka International journal of impact engineering 26 (1-10), 13-19, 2001 | 24 | 2001 |
Development of perforation hole detection system for space debris impact S Fukushige, Y Akahoshi, T Koura, S Harada International journal of impact engineering 33 (1-12), 273-284, 2006 | 20 | 2006 |
Investigation and comparison between new satellite impact test results and NASA standard breakup model K Sakuraba, Y Tsuruda, T Hanada, JC Liou, Y Akahoshi International journal of impact engineering 35 (12), 1567-1572, 2008 | 19 | 2008 |
Meaurement of mass. spray angle and velocity distribution of fragment cloud Y Akahoshi, Y Kaji, H Hata International journal of impact engineering 29 (1-10), 845-853, 2003 | 19 | 2003 |
Debris cloud distributions at oblique impacts M Higashide, T Koura, Y Akahoshi, S Harada International Journal of Impact Engineering 35 (12), 1573-1577, 2008 | 18 | 2008 |
Fracture parameter for molecular dynamics method H Inoue, Y Akahoshi, S Harada International journal of fracture 66 (4), R77-R81, 1994 | 17 | 1994 |
Intact measurement of fragments in ejecta due to hypervelocity impact K Sugahara Proc. 60th Int. Astronautical Cong., 2009, 2009 | 13 | 2009 |
Using NASA standard breakup model to describe low-velocity impacts on spacecraft T Hanada, T Yasaka, H Hata, Y Akahoshi Journal of spacecraft and rockets 42 (5), 859-864, 2005 | 13 | 2005 |
Low-velocity catastrophic impact on micro satellite K Nakashima, T Hanada, Y Akahoshi, T Harano, Y Machida, S Fukushige Proceedings of the 4th European Conference on Space Debris, ESOC, Darmstadt …, 2005 | 11 | 2005 |
Construction of mass, three-dimensional and velocity distribution for the second debris clouds Y Akahoshi, T Nakamura International journal of impact engineering 26 (1-10), 1-11, 2001 | 9 | 2001 |
A molecular dynamics-aided fracture mechanics parameter and its application to a tensile problem H Inoue, Y Akahoshi, S Harada Computational mechanics 16 (4), 217-222, 1995 | 9 | 1995 |