Assessing possible mutual orbit period change by shape deformation of Didymos after a kinetic impact in the NASA-led Double Asteroid Redirection Test

被引:23
|
作者
Hirabayashi, Masatoshi [1 ]
Davis, Alex B. [2 ]
Fahnestock, Eugene G. [3 ]
Richardson, Derek C. [4 ]
Michel, Patrick [5 ]
Cheng, Andrew F. [6 ]
Rivkin, Andrew S. [6 ]
Scheeres, Daniel J. [2 ]
Chesley, Steven R. [3 ]
Yu, Yang [7 ]
Naidu, Shantanu P. [3 ]
Schwartz, Stephen R. [8 ]
Benner, Lance A. M. [3 ]
Pravec, Petr [9 ]
Stickle, Angela M. [6 ]
Jutzi, Martin [10 ]
机构
[1] Auburn Univ, 319 Davis Hall, Auburn, AL 36849 USA
[2] Univ Colorado, 429 UCB, Boulder, CO 80309 USA
[3] CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
[4] Univ Maryland, College Pk, MD 20742 USA
[5] Univ Cote Azur, CNRS, Observ Cote Azur, Lab Lagrange, CS 34229, F-06304 Nice 4, France
[6] Johns Hopkins Univ, Appl Phys Lab, Johns Hopkins Rd, Laurel, MD 20723 USA
[7] Beihang Univ, Beijing 100191, Peoples R China
[8] Univ Arizona, Tempe, AZ 85287 USA
[9] Acad Sci Czech Republ, Astron Inst, Fricova 1, CZ-25165 Ondrejov, Czech Republic
[10] Univ Bern, Phys Inst, Space Res & Planetary Sci, Sidlerstr 5, CH-3012 Bern, Switzerland
基金
美国国家科学基金会;
关键词
Planetary defense; Asteroid impact hazards; Kinetic impactor; Mutual orbit dynamics; Binary asteroids; 2 RIGID BODIES; NUMERICAL SIMULATIONS; ROTATIONAL BREAKUP; EJECTA CLOUD; DEFLECTION; STABILITY; DISRUPTION; EVOLUTION; SECONDARY; BODY;
D O I
10.1016/j.asr.2018.12.041
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The Asteroid Impact & Deflection Assessment (AIDA) targets binary near-Earth asteroid (65803) Didymos. As part of this mission, the NASA-led Double Asteroid Redirection Test (DART) will make a kinetic impactor collide with the smaller secondary of Didymos to test kinetic impact asteroid deflection technology, while the ESA-led Hera mission will evaluate the efficiency of the deflection by conducting detailed on-site observations. Research has shown that the larger primary of Didymos is spinning close to its critical spin, and the DART-impact-driven ejecta would give kinetic energy to the primary. It has been hypothesized that such an energy input might cause structural deformation of the primary, affecting the mutual orbit period, a critical parameter for assessing the kinetic impact deflection by the DART impactor. A key issue in the previous work was that the secondary was assumed to be spherical, which may not be realistic. Here, we use a second-order inertia-integral mutual dynamics model to analyze the effects of the shapes of the primary and the secondary on the mutual orbit period change of the system. We first compare the second-order model with three mutual dynamics models, including a high-order inertia-integral model that takes into account the detailed shapes of Didymos. The comparison tests show that the second-order model may have an error of similar to 10% for computing the mutual orbit period change, compared to the high-order model. We next use the second-order model to analyze how the original shape and shape deformation change the mutual orbit period. The results show that when the secondary is elongated, the mutual orbit period becomes short. Also, shape deformation of the secondary further changes the mutual orbit period. A better understanding of this mechanism allows for detailed assessment of DART's kinetic impact deflection capability for Didymos. (C) 2019 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:2515 / 2534
页数:20
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