Optimal Kinetic-Impact Geometry for Asteroid Deflection Exploiting Delta-V Hodograph

被引:4
|
作者
Jiao, Yifei [1 ]
Cheng, Bin [1 ]
Baoyin, Hexi [1 ,2 ]
机构
[1] Tsinghua Univ, Sch Aerosp Engn, Beijing 100084, Peoples R China
[2] Inner Mongolia Univ Technol, Hohhot 010051, Inner Mongolia, Peoples R China
基金
国家重点研发计划;
关键词
MOMENTUM-TRANSFER; EJECTA PLUME; DESIGN; MODEL;
D O I
10.2514/1.G006876
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:382 / 389
页数:8
相关论文
共 3 条
  • [1] Deflection by kinetic impact: Sensitivity to asteroid properties
    Syal, Megan Bruck
    Owen, J. Michael
    Miller, Paul L.
    ICARUS, 2016, 269 : 50 - 61
  • [2] 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
  • [3] 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)