• 제목/요약/키워드: (99942) Apophis

검색결과 3건 처리시간 0.054초

A Preliminary Impulsive Trajectory Design for (99942) Apophis Rendezvous Mission

  • Kim, Pureum;Park, Sang-Young;Cho, Sungki;Jo, Jung Hyun
    • Journal of Astronomy and Space Sciences
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    • 제38권2호
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    • pp.105-117
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    • 2021
  • In this study, a preliminary trajectory design is conducted for a conceptual spacecraft mission to a near-Earth asteroid (NEA) (99942) Apophis, which is expected to pass by Earth merely 32,000 km from the Earth's surface in 2029. This close approach event will provide us with a unique opportunity to study changes induced in asteroids during close approaches to massive bodies, as well as the general properties of NEAs. The conceptual mission is set to arrive at and rendezvous with Apophis in 2028 for an advanced study of the asteroid, and some near-optimal (in terms of fuel consumption) trajectories under this mission architecture are to be investigated using a global optimization algorithm called monotonic basin hopping. It is shown that trajectories with a single swing-by from Venus or Earth, or even simpler ones without gravity assist, are the most feasible. In addition, launch opportunities in 2029 yield another possible strategy of leaving Earth around the 2029 close approach event and simply following the asteroid thereafter, which may be an alternative fuel-efficient option that can be adopted if advanced studies of Apophis are not required.

Apophis Rendezvous Mission: I. Science Goals

  • Kim, Myung-Jin;Moon, Hong-Kyu;Choi, Young-Jun;Jeong, Minsup;Choi, Jin;JeongAhn, Youngmin;Yang, Hongu;Baek, Seul-Min;Lee, Hee-Jae;Ishiguro, Masateru
    • 천문학회보
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    • 제46권1호
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    • pp.43.4-44
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    • 2021
  • 99942 Apophis is an Sq-type Aten group Near-Earth Asteroid (NEA) with an estimated size of 370 m. It will approach the Earth to come within the geostationary orbit during the upcoming encounter on April 13, 2029 to offer a unique chance to study its 1) global properties, 2) surface arrangements, and 3) their detectable changes expected to happen, in sub-meter scale. What measurable scientific goals for the asteroid in this "once a millennium" event could transform our knowledge of planetary science and defense? The Apophis rendezvous mission aims to understand the characteristics of the small solar system body's nature. It also prepares for potential threats from natural objects by measuring in-situ surface, shape, rotation, and orbit changes expected to occur when the target asteroid passes close to the Earth in 2029. We will present an overview of the mission scheduled to be launched from late 2026 to early 2027 and introduce scientific objectives.

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Rendezvous Mission to Apophis: II. Science Goals

  • Kim, Myung-Jin;Moon, Hong-Kyu;Choi, Young-Jun;Jeong, Minsup;Ishiguro, Masateru;JeongAhn, Youngmin;Lee, Hee-Jae;Yang, Hongu;Baek, Seul-Min;Choi, Jin;Sim, Chae Kyung;Lee, Dukhang;Kim, Dong-Heun;Cho, Eunjin;Lee, Mingyeong;Bach, Yoonsoo;Jin, Sunho;Geem, Jooyeon;Jo, Hangbin;Choi, Sangho;Kim, Yaeji;Kim, Yoonyoung;Kwon, Yuna
    • 천문학회보
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    • 제46권2호
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    • pp.57.3-57.3
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    • 2021
  • 99942 Apophis is an Sq-type Potentially Hazardous Asteroid (PHA) with an estimated diameter of 370 m. It will approach the Earth down to 31,000 km from the surface during the encounter on April 13, 2029 UT, which is closer than geostationary satellites. This once-in-a-20,000 year opportunity would further expand our knowledge on the physical and dynamical processes which are expected to occur due to the gravitational tidal forces when an asteroid encounter with a planet. It will also provide an opportunity to promote great knowledge of the science of planetary defense. The science goal of the Apophis mission is to global-map the asteroid before and after the Earth's approach. In this talk, we will present scientific objectives, and briefly introduce instruments and operation scenarios of the mission.

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