Yinghuo-1 (simplified Chinese: 萤火一号; traditional Chinese: 螢火一號; pinyin: Yínghuǒ yī hào) was a Chinese Mars-explorationspace probe, intended to be the first Chinese planetary space probe and the first Chinese spacecraft to orbit Mars. It was launched from Baikonur Cosmodrome, Kazakhstan, on 8 November 2011, along with the RussianFobos-Gruntsample return spacecraft, which was intended to visit Mars' moon Phobos.[2][6] The 115-kg (250-lb) Yinghuo-1 probe was intended by the CNSA to orbit Mars for about two years,[1] studying the planet's surface, atmosphere, ionosphere and magnetic field.[citation needed] Shortly after launch, Fobos-Grunt was expected to perform two burns to depart Earth orbit bound for Mars. However, these burns did not take place, leaving both probes stranded in orbit.[7] On 17 November 2011, CNSA reported that Yinghuo-1 had been declared lost.[8] After a period of orbital decay, Yinghuo-1 and Fobos-Grunt underwent destructive re-entry on 15 January 2012, finally disintegrating over the Pacific Ocean.[5][9]
As a result, CNSA subsequently moved to embark on an independent Mars exploration program, which culminated in the Tianwen-1 orbiter-lander-rover mission that successfully landed the Zhurong rover on Mars on 22 May, 2021.[10]
On 26 March 2007, the director of the China National Space Administration, Sun Laiyan, and the head of the Russian Space Agency, Anatoly Perminov, signed a landmark space co-operation accord, entitled the "Cooperative Agreement between the China National Space Administration and the Russian Space Agency on joint Chinese-Russian exploration of Mars". One stipulation of the agreement was the construction and launch of the Yinghuo Mars orbiter and its Russian counterpart, Fobos-Grunt.[4]
Instruments and objectives
Yinghuo-1's primary scientific objectives were:
To conduct detailed investigation of the plasma environment and magnetic field around Mars.
To study Martian ion escape processes and their possible mechanisms
To conduct ionosphere occultation measurements between Yinghuo-1 and Fobos-Grunt, focusing on the sub-solar and midnight regions.
An optical imaging system consisting of two cameras with 200 m (660 ft) resolution for high-quality images of the Martian surface to be captured from orbit.
Mission profile
Diagram showing Yinghuo-1's intended approach pathway to Mars.
Following its transit to Mars, Yinghuo-1 was planned to separate from Fobos-Grunt in October 2012[13] and enter a 72.8-hour equatorial Martian orbit,[1] with an orbital inclination of approximately 5 degrees.[citation needed] Fobos-Grunt and Yinghuo-1 would have conducted Mars ionosphereoccultation experiments together,[14] although Fobos-Grunt's primary objective was to obtain surface samples from the Martian moon Phobos. Yinghuo-1 would have experienced periods of up to 8.8 hours in darkness when its orbit carried it over Mars' nightside; it would have run on battery power during these periods, as its solar panels would have been unusable without direct sunlight.[1]
Launch processing
On 17 October 2011, the completed Yinghuo-1 satellite arrived at Baikonur Cosmodrome with Fobos-Grunt, beginning payload processing operations in preparation for its November launch.[15]
Launch and orbital burn failure
China's Yinghuo-1 and the Russian Fobos-Grunt spacecraft were launched together aboard a UkrainianZenit rocket with a Fregat upper stage from Baikonur Cosmodrome, Kazakhstan, on 8 November 2011.[2][13] Shortly after launch, Fobos-Grunt was expected to perform two burns to depart Earth orbit and begin its journey to Mars. However, these burns did not take place, stranding the two spacecraft in their parking orbit.[16] Despite repeated efforts to contact the launcher and rectify the problem, the spacecraft continued to lose altitude.[17] On 17 November, Chinese state media formally declared the Yinghuo-1 probe lost,[8] and the launcher's orbit gradually began to decay.
Destructive re-entry
On 14 January 2012, it was reported that Fobos-Grunt and Yinghuo-1 were beginning their final descent into Earth's atmosphere, falling at a rate of several hundred metres per hour from their 147-kilometre (91 mi) orbital altitude.[9] The two spacecraft completed their re-entry and disintegrated over the Pacific Ocean on 15 January 2012.[5]
Specifications
Length: 0.75 metres (2.5 ft) (excluding solar panels).[18]
Power: 3-axis stabilised, 2×3 section solar array with a full-extended length of 5.6 metres (18 ft), providing average power of 90 W, and peak power of 180 W.[14]
HGA: 950 mm antenna dish (S-band) with a 12 W transmitter in two frequencies (8.4 and 7.17 GHz) and a data rate between 8 bit/s and 16 kbit/s.[14]
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Cubesats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Various conventions, treaties, agreements, memorandums, charters or declarations establishing and governing intergovernmental organisations or inter-agency bodies dealing with space affairs
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