On the Characteristics of Singular Trajectories of the Asteroid Apophis and the Possibility of Deflecting It to Avoid Collisions with the Earth

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On the Characteristics of Singular Trajectories of the Asteroid Apophis and the Possibility of Deflecting It to Avoid Collisions with the Earth. / Sokolov, L. L.; Kuteeva, G. A.; Petrov, N. A.; Eskin, B. B.; Balyaev, I. A.; Vasil’ev, A. A.

в: Solar System Research, Том 55, № 3, 05.2021, стр. 259-265.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

BibTeX

@article{abdc3aed81fa40a89d31334fa79fc94f,

title = "On the Characteristics of Singular Trajectories of the Asteroid Apophis and the Possibility of Deflecting It to Avoid Collisions with the Earth",

abstract = "Analysis is conducted of the asteroid Apophis' approaches to the Earth on potential collision trajectories. Close approaches, especially in 2051, allow the use of the gravity assist effect to deflect the asteroid at small energy costs. Estimates are obtained for the change in Apophis' velocity after 2029, which are required to divert the object and avoid its main possible collisions with the Earth.",

keywords = "asteroid, collision orbit, resonant returns, IMPACT TRAJECTORIES, MOTION, ORBIT CORRECTION",

author = "Sokolov, {L. L.} and Kuteeva, {G. A.} and Petrov, {N. A.} and Eskin, {B. B.} and Balyaev, {I. A.} and Vasil{\textquoteright}ev, {A. A.}",

note = "Publisher Copyright: {\textcopyright} 2021, Pleiades Publishing, Inc.",

year = "2021",

month = may,

doi = "10.1134/s0038094621010093",

language = "English",

volume = "55",

pages = "259--265",

journal = "Solar System Research",

issn = "0038-0946",

publisher = "МАИК {"}Наука/Интерпериодика{"}",

number = "3",

}

RIS

TY - JOUR

T1 - On the Characteristics of Singular Trajectories of the Asteroid Apophis and the Possibility of Deflecting It to Avoid Collisions with the Earth

AU - Sokolov, L. L.

AU - Kuteeva, G. A.

AU - Petrov, N. A.

AU - Eskin, B. B.

AU - Balyaev, I. A.

AU - Vasil’ev, A. A.

PY - 2021/5

Y1 - 2021/5

N2 - Analysis is conducted of the asteroid Apophis' approaches to the Earth on potential collision trajectories. Close approaches, especially in 2051, allow the use of the gravity assist effect to deflect the asteroid at small energy costs. Estimates are obtained for the change in Apophis' velocity after 2029, which are required to divert the object and avoid its main possible collisions with the Earth.

AB - Analysis is conducted of the asteroid Apophis' approaches to the Earth on potential collision trajectories. Close approaches, especially in 2051, allow the use of the gravity assist effect to deflect the asteroid at small energy costs. Estimates are obtained for the change in Apophis' velocity after 2029, which are required to divert the object and avoid its main possible collisions with the Earth.

KW - asteroid

KW - collision orbit

KW - resonant returns

KW - IMPACT TRAJECTORIES

KW - MOTION

KW - ORBIT CORRECTION

UR - http://www.scopus.com/inward/record.url?scp=85110450166&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/381ce6e9-547b-3f7a-81b6-e70b19efc6bd/

U2 - 10.1134/s0038094621010093

DO - 10.1134/s0038094621010093

M3 - Article

AN - SCOPUS:85110450166

VL - 55

SP - 259

EP - 265

JO - Solar System Research

JF - Solar System Research

SN - 0038-0946

IS - 3

ER -

ID: 84311627