The Double Asteroid Redirection Test Mission

被引:0
|
作者
Kantsiper, Brian [1 ]
Cheng, Andy [1 ]
Reed, Cheryl [1 ]
机构
[1] Johns Hopkins Univ, Appl Phys Lab, 11100 Johns Hopkins Rd, Laurel, MD 20723 USA
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
U.S. Government work not protected by U.S. copyright On Feb. 15, 2013, a 20-meter asteroid unexpectedly hit the Earth without any warning near Chelyabinsk, Russia. This impact released about 500 kilotons TNT of energy, injured over 1500 people, and caused extensive property damage. The Chelyabinsk impact served as a dramatic reminder of the asteroid impact hazard and re-emphasized the importance of discovering hazardous Near Earth Objects (NEOs) and learning how to mitigate the threat they pose. Mitigation of a hazardous NEO can be accomplished by deflecting it so that it misses the Earth. Strategies to deflect an asteroid include impacting it with a spacecraft (a kinetic impactor), pulling it with the gravity of the mass of a spacecraft (a gravity tractor), using the blast of a nearby nuclear explosion, and modifying the surface or causing ablation by various means including lasers or particle beams. None of these approaches has been tested on a NEO. The AIDA mission is a proposed international collaboration to demonstrate kinetic deflection, the most mature technique for mitigating the impact hazard of a Near Earth Object (NEO). AIDA consists of two mission elements, the NASA Double Asteroid Redirection Test (DART) mission and the ESA Asteroid Impact Mission (AIM). The main objectives of the DART mission, which includes the spacecraft kinetic impact and an Earth-based observing campaign, are to: Perform a full scale demonstration of the spacecraft kinetic impact technique for deflection of an asteroid, by targeting an object large enough to qualify as a Potentially Hazardous Asteroid; Measure the resulting asteroid deflection, by targeting the secondary member of a binary NEO and measuring the period change of the binary orbit; Understand the hypervelocity collision effects on an asteroid, including the long-term dynamics of impact ejecta; validate models for momentum transfer in asteroid impacts, inferring physical properties of the asteroid surface and sub-surface. The DART target is the secondary member of the binary asteroid 65803 Didymos, with the impact scheduled to occur in September, 2022. The DART impact on the secondary member of the Didymos binary at similar to 7 km/s will alter the binary orbit period by at least 4 minutes, assuming a simple transfer of momentum to the target. The period change may be significantly greater, as the momentum transferred to the target asteroid may exceed the incident momentum of the U.S. Government work not protected by U.S. copyright kinetic impactor, possibly by a large factor. The AIM spacecraft will characterize the asteroid target and monitor results of the impact in situ at Didymos, but the period change can be determined accurately solely with ground-based observatories, an approach that is only feasible because of the choice of a binary system as target. AIM is currently in Phase A. DART held its Mission Concept Review on May 21-22, 2015. This paper summarizes the DART mission concept and the path forward in Phase A.
引用
收藏
页数:6
相关论文
共 50 条
  • [31] Near to Mid-infrared Spectroscopy of (65803) Didymos as Observed by JWST: Characterization Observations Supporting the Double Asteroid Redirection Test
    Rivkin, Andrew S.
    Thomas, Cristina A.
    Wong, Ian
    Rozitis, Benjamin
    de Leon, Julia
    Holler, Bryan
    Milam, Stefanie N.
    Howell, Ellen S.
    Hammel, Heidi B.
    Arredondo, Anicia
    Brucato, John R.
    Epifani, Elena M.
    Ieva, Simone
    La Forgia, Fiorangela
    Lucas, Michael P.
    Lucchetti, Alice
    Pajola, Maurizio
    Poggiali, Giovanni
    Sunshine, Jessica N.
    Trigo-Rodriguez, Josep M.
    PLANETARY SCIENCE JOURNAL, 2023, 4 (11):
  • [32] NASA's Double Asteroid Redirection Test (DART): Mutual Orbital Period Change Due to Reshaping in the Near-Earth Binary Asteroid System (65803) Didymos
    Nakano, Ryota
    Hirabayashi, Masatoshi
    Agrusa, Harrison F.
    Ferrari, Fabio
    Meyer, Alex J.
    Michel, Patrick
    Raducan, Sabina D.
    Sanchez, Paul
    Zhang, Yun
    PLANETARY SCIENCE JOURNAL, 2022, 3 (07):
  • [33] Concurrent Redirection and Attitude Control of an Asteroid
    Bazzocchi, Michael C. F.
    Emami, M. Reza
    2019 IEEE AEROSPACE CONFERENCE, 2019,
  • [34] MISSION TO AN ASTEROID
    ALFVEN, H
    ARRHENIUS, G
    SCIENCE, 1970, 167 (3915) : 139 - +
  • [35] ASTEROID MISSION
    Murphy, Steve
    SCIENTIFIC AMERICAN, 2016, 315 (06) : 8 - 8
  • [36] Femtosecond Optical Metrology Applied to Asteroid Redirection
    Fork, R. L.
    2017 CONFERENCE ON LASERS AND ELECTRO-OPTICS EUROPE & EUROPEAN QUANTUM ELECTRONICS CONFERENCE (CLEO/EUROPE-EQEC), 2017,
  • [37] Explaining the asteroid mission
    Jones, Tom
    AEROSPACE AMERICA, 2014, 52 (06) : 12 - 14
  • [38] DART mission deflects asteroid in first-of-its-kind test
    Banks, Michael
    PHYSICS WORLD, 2022, 35 (11) : 13 - +
  • [39] Assessing possible mutual orbit period change by shape deformation of Didymos after a kinetic impact in the NASA-led Double Asteroid Redirection Test
    Hirabayashi, Masatoshi
    Davis, Alex B.
    Fahnestock, Eugene G.
    Richardson, Derek C.
    Michel, Patrick
    Cheng, Andrew F.
    Rivkin, Andrew S.
    Scheeres, Daniel J.
    Chesley, Steven R.
    Yu, Yang
    Naidu, Shantanu P.
    Schwartz, Stephen R.
    Benner, Lance A. M.
    Pravec, Petr
    Stickle, Angela M.
    Jutzi, Martin
    ADVANCES IN SPACE RESEARCH, 2019, 63 (08) : 2515 - 2534
  • [40] Comparative analysis of redirection methods for asteroid resource exploitation
    Bazzocchi, Michael C. F.
    Emami, M. Reza
    ACTA ASTRONAUTICA, 2016, 120 : 1 - 19