Английская Википедия:DESTINY+

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Шаблон:Short description Шаблон:Use American English Шаблон:Use dmy dates Шаблон:Infobox spaceflight

DESTINY+ (Demonstration and Experiment of Space Technology for INterplanetary voYage with Phaethon fLyby and dUst Science) is a planned mission to flyby the Geminids meteor shower parent body 3200 Phaethon, and sample dust originating from the "rock comet".[1] The spacecraft is being developed by the Japanese space agency JAXA, and will demonstrate advanced technologies for future deep space exploration. As of 2023, DESTINY+ is planned to be launched in 2025.[2]

Overview

DESTINY+ will be launched from Uchinoura Space Center by an Epsilon S launch vehicle into low Earth orbit, and will spend 1.5 years raising its orbit with ion engines.[3] A lunar flyby (at ~Шаблон:Cvt) will accelerate the probe into an interplanetary orbit. During this cruise time it will fly by a few near Earth objects for study, including the transition body 3200 Phaethon in 2029, as well as measure interplanetary and interstellar dust.[4][5]

The probe's ion engines have the capability to perform another orbit transfer to study additional objects.[6]

Objectives

DESTINY+ will be a technology demonstrator to further improve operations of low cost solar electric propulsion in deep space. It will also demonstrate innovative light-weight solar array panel technology. The scientific aspect of this mission is to understand origin and nature of dusts, which are key sources of organic compounds to Earth. It will also observe dusts from comet/asteroid 3200 Phaethon using a dust analyzer and will map its surface using a multiband telescopic camera to understand the mechanisms of dust ejection.[3] The spacecraft will come as close as Шаблон:Cvt from 3200 Phaethon.[3]

Spacecraft

DESTINY+ will use ultra light-weight solar panels and heat-actuated folding radiators, along with compact avionics. The spacecraft is designed to tolerate a radiation dose up to approximately 30 krad by using a 3 mm aluminum shield.[3]

Propulsion

The spacecraft will be propelled by four μ10 solar electric ion engines,[3] as used by Hayabusa and Hayabusa2, but while its predecessors operated only up to three engines simultaneously, DESTINY+ will use all four simultaneously [7] for a total thrust of 40 mN (specific impulse: 3000 seconds; acceleration: 83 μm/s2; power: 1670 watts.[3]) The total dry mass (excludes xenon propellant) of the ion engine system is Шаблон:Cvt.[3]

Payload

DESTINY PLUS will carry three scientific instruments:[4]

  • DESTINY Dust Analyzer (DDA) — The DESTINY Dust Analyzer (2.7 kg) will be provided by the German Aerospace Center (DLR),[8] and is being developed by the University of Stuttgart.[3][9]
  • Telescopic Camera for Phaethon (TCAP) — The telescopic camera has a mass of 15.8 kg.[3]
  • Multiband Camera for Phaethon (MCAP) — The multiband camera has a mass of 3.5 kg and will detect light in 390 nm, 550 nm, 700 nm, 850 nm wavelengths.[3]

See also

Шаблон:Portal

References

Шаблон:Reflist

External links

Шаблон:Asteroid spacecraft Шаблон:Japanese space program Шаблон:Future spaceflights

  1. Шаблон:Cite book
  2. Ошибка цитирования Неверный тег <ref>; для сносок space-20231106 не указан текст
  3. 3,0 3,1 3,2 3,3 3,4 3,5 3,6 3,7 3,8 3,9 Шаблон:Cite web
  4. 4,0 4,1 Studies on Solar System Explorations using DESTINY: the Demonstration and Experiment of Space Technology for Interplanetary Voyage Takahiro Iwata, Yasuhiro Kawakatsu, Go Murakami, Yuichiro Ezoe, Shingo Kameda, Kunihiro Keika, Tomoko Arai, Shuji Matsuura, Takanao Saiki, Takeshi Imamura, Kazunori Ogohara, Akira Oyama, Toshinori Ikenaga; ISTS Special Issue: Selected papers from the 30th International Symposium on Space Technology and Science Vol. 14 (2016) No. ists30; DOI: http://doi.org/10.2322/tastj.14.Pk_111
  5. Шаблон:Cite conference
  6. DESTINY Mission Overview Yasuhiro KAWAKATSU JAXA
  7. Шаблон:Cite web
  8. Шаблон:Cite press release
  9. Шаблон:Cite web