Study of the effects of projectile strength and density in the asteroid deflection by hypervelocity impact

被引:2
|
作者
Wakatsuki, Yusuke [1 ]
Akahoshi, Yasuhiro [1 ]
Koura, Takao [1 ]
Takahara, Hiroki [1 ]
机构
[1] Kyushu Inst Technol, Dept Space Syst Engn, 1-1 Sensui Cho,Tobata Ku, Kitakyushu, Fukuoka 8048550, Japan
关键词
Momentum enhancement factor; Two-stage light gas gun; ANSYS AUTODYN; Impact scale; Crater shape; MOMENTUM-TRANSFER; OBLIQUE IMPACTS;
D O I
10.1016/j.ijimpeng.2023.104710
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In recent years, potentially hazardous asteroids (PHAs), which have orbits approaching the Earth and are a threat to humankind, have been attracting attention. It is necessary to prevent them from impacting the Earth, and asteroid deflection by hypervelocity impact is one of the best impact avoidance. This asteroid deflection needs to be greater, but momentum enhancement factor /%, which represents deflection efficiency, is affected by various factors. This study focused on projectile strength and density, and experiments for small-scale impacts and numerical simulations for large-scale impacts were conducted to clarify these effects on /%. In experiments, six types of projectiles with different strengths and densities and the same shape and size were impacted into brick targets at 1-3.5 km/s using a Two-Stage Light Gas Gun to investigate the effects in actual impacts. In simulations, three types of projectiles with different densities and the same shape and mass were impacted into granite targets at 310 km/s using AUTODTN to investigate the effects in asteroid-deflection-scale impacts, which are difficult for experiments. In conclusion, the effect of projectile strength on /% is less, and the one of projectile density on /% is high. It is demonstrated that projectiles whose density is close to the target density increase /%, namely, are suitable for asteroid deflection regardless of impact scale. Additionally, a crater formed by hypervelocity impact is a preferably flat shape for asteroid deflection, and the effect of crater shape on /% is higher at large-scale impact. Further study of this effect and the scaling one could be expected.
引用
收藏
页数:11
相关论文
共 18 条
  • [1] Study of the Effects of Projectile Shape in the Asteroid Orbit Change by Spacecraft Impact
    Ikeda, Masaya
    Tanaka, Masashi
    Yokoo, Daisuke
    Koura, Takao
    Akahoshi, Yasuhiro
    14TH HYPERVELOCITY IMPACT SYMPOSIUM (HVIS 2017), 2017, 204 : 138 - 145
  • [2] Effects of projectile parameters on the momentum transfer and projectile melting during hypervelocity impact
    Liu, Wenjin
    Zhang, Qingming
    Long, Renrong
    Gong, Zizheng
    Jiankang, Ren
    Hu, Xin
    Ren, Siyuan
    Wu, Qiang
    Song, Guangming
    DEFENCE TECHNOLOGY, 2024, 32 : 89 - 103
  • [3] Deflection by kinetic impact: Sensitivity to asteroid properties
    Syal, Megan Bruck
    Owen, J. Michael
    Miller, Paul L.
    ICARUS, 2016, 269 : 50 - 61
  • [4] Asteroid Impact and Deflection Assessment mission
    Cheng, A. F.
    Atchison, J.
    Kantsiper, B.
    Rivkin, A. S.
    Stickle, A.
    Reed, C.
    Galvez, A.
    Carnelli, I.
    Michel, P.
    Ulamec, S.
    ACTA ASTRONAUTICA, 2015, 115 : 262 - 269
  • [5] Hypervelocity impact cratering of chondritic meteorites: Implications for asteroid recoil
    Flynn, G. J.
    Durda, D. D.
    Patmore, E. B.
    Jack, S. J.
    Molesky, M. J.
    May, B. A.
    Strait, M. M.
    Macke, R. J.
    14TH HYPERVELOCITY IMPACT SYMPOSIUM (HVIS 2017), 2017, 204 : 146 - 153
  • [6] Asteroid Impact & Deflection Assessment mission: Kinetic impactor
    Cheng, A. F.
    Michel, R.
    Jutzi, M.
    Rivkin, A. S.
    Stickle, A.
    Barnouin, O.
    Ernst, C.
    Atchison, J.
    Pravec, P.
    Richardson, D. C.
    PLANETARY AND SPACE SCIENCE, 2016, 121 : 27 - 35
  • [7] Science case for the Asteroid Impact Mission (AIM): A component of the Asteroid Impact & Deflection Assessment (AIDA) mission
    Michel, Patrick
    Cheng, A.
    Kueppers, M.
    Pravec, P.
    Blum, J.
    Delbo, M.
    Green, S. F.
    Rosenblatt, P.
    Tsiganis, K.
    Vincent, J. B.
    Biele, J.
    Ciarletti, V.
    Herique, A.
    Ulamec, S.
    Carnelli, I.
    Galvez, A.
    Benner, L.
    Naidu, S. P.
    Barnouin, O. S.
    Richardson, D. C.
    Rivkin, A.
    Scheirich, P.
    Moskovitz, N.
    Thirouin, A.
    Schwartz, S. R.
    Campo Bagatin, A.
    Yu, Y.
    ADVANCES IN SPACE RESEARCH, 2016, 57 (12) : 2529 - 2547
  • [8] Gravitational perturbations correlated with the asteroid kinetic impact deflection technique
    Chagas, B. S.
    Prado, A. F. B. A.
    Winter, O. C.
    SCIENTIFIC REPORTS, 2022, 12 (01)
  • [9] Deflection driven evolution of asteroid impact risk under large uncertainties
    Rumpf, Clemens M.
    Mathias, Donovan L.
    Wheeler, Lorien F.
    Dotson, Jessie L.
    Barbee, Brent
    Roa, Javier
    Chodas, Paul
    Farnocchia, Davide
    ACTA ASTRONAUTICA, 2020, 176 (176) : 276 - 286
  • [10] Post mitigation impact risk analysis for asteroid deflection demonstration missions
    Eggl, Siegfried
    Hestroffer, Daniel
    Thuillot, William
    Bancelin, David
    Cano, Juan L.
    Cichocki, Filippo
    ADVANCES IN SPACE RESEARCH, 2015, 56 (03) : 528 - 548