Cheng, A.F. und Michel, P. und Barnouin, O.S. und Campo-Bagatin, A. und Miller, P. und Pravec, P. und Richardson, D. C. und Rivkin, A. S. und Schwartz, S. R. und Stickel, A. und Tsiganis, K. und Ulamec, S. (2016) Asteroid Impact and Deflection Assessment (AIDA) Mission: The double Asteroid redirection test (DART). 47th Lunar an dPlanetary Science Conference, 2016-03-21 - 2016-03-25, The Woodlands, TX - USA.
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Kurzfassung
The Asteroid Impact & Deflection Assessment (AIDA) mission will be the first space experiment to demonstrate asteroid impact hazard mitigation by using a kinetic impactor. AIDA is a joint ESA-NASA cooperative project [1,2], that includes the ESA Asteroid Impact Mission (AIM) rendezvous spacecraft and the NASA Double Asteroid Redirection Test (DART) mission. The AIDA target is the near- Earth binary asteroid 65803 Didymos, which will make an unusually close approach to Earth in October, 2022. The ~300-kg DART spacecraft is designed to impact the Didymos secondary at 7 km/s and demon- strate the ability to modify its trajectory through momentum transfer. DART and AIM are currently Phase A studies supported by NASA and ESA respectively. The primary goals of AIDA are (1) perform a full-scale demonstration of the spacecraft kinetic impact technique for deflection of an asteroid, by targeting an object larger than ~100 m and large enough to qualify as a Potentially Hazardous Asteroid; (2) measure the resulting asteroid deflection, by targeting the second- ary member of a binary NEO and measuring the period change of the binary orbit; (3) understand the hypervelocity collision effects on an asteroid, including the long-term dynamics of impact ejecta; and validate models for momentum transfer in asteroid impacts, based on measured physical properties of the asteroid surface and sub-surface. The primary DART objectives are to demonstrate a hypervelocity impact on the Did- ymos moon and to determine the resulting deflection from ground-based observatories. The DART impact on the Didymos secondary will cause a measurable change in the orbital period of the binary. The AIM spacecraft will be launched in Dec. 2020 and arrive at Didymos in spring, 2022, several months before the DART impact. AIM will characterize the Didymos binary system by means of remote sensing and in-situ instruments both before and after the DART impact. The asteroid deflection will be meas- ured to higher accuracy, and additional results of the DART impact, like the impact cater, will be studied in great detail by the AIM mission.
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Titel: | Asteroid Impact and Deflection Assessment (AIDA) Mission: The double Asteroid redirection test (DART) | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | 21 März 2016 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Referierte Publikation: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Stichwörter: | AIDA, DART | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungstitel: | 47th Lunar an dPlanetary Science Conference | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsort: | The Woodlands, TX - USA | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsbeginn: | 21 März 2016 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsende: | 25 März 2016 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstalter : | USRA | ||||||||||||||||||||||||||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||||||||||||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||||||||||||||||||||||||||||||||||||||
HGF - Programmthema: | Erforschung des Weltraums | ||||||||||||||||||||||||||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||||||||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | R EW - Erforschung des Weltraums | ||||||||||||||||||||||||||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Explorationsstudien (alt) | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Standort: | Köln-Porz | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Raumflugbetrieb und Astronautentraining > Nutzerzentrum für Weltraumexperimente (MUSC) | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Hinterlegt von: | Herrmann, Astrid | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Hinterlegt am: | 30 Mär 2016 10:20 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:09 |
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