Image:From Mission Concept to Mars Orbit.pdf
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[edit] Summary
Mars Express, ESA's first mission to orbit another planet, was launched on 2 June 2003 and arrived at Mars on 25 December 2003. Since orbit insertion it has successfully imaged more than 45% of Mars in infra-red and visible spectrums at resolutions of 10-100m/pixel, and returned extensive spectrometric science data for the planet’s atmosphere and surface, and Mars’ moon Phobos. The nominal mission ended November 2005 and a first extension will be completed end October 2007. Mars Express has also demonstrated data-relay capability for uplink/downlink to NASA MER rovers. The original mission operations concept was constrained partly by the resources available from a spacecraft designed within a very tight “flexi-class” mission budget. The major trade-off was between exploiting each pericenter pass for science, and the original concept of a single, daily, communications pass over the New Norcia ESA 35m deep-space antenna. An agreement was reached with NASA to provide pass-time on 34m and 70m antennas of the deep-space network, to provide additional downlink time and minimize pericenters lost for science. A fault in the power system, detected only after launch, left Mars Express limited to a maxi mum availability of 70% of design power for the entire mission. With long eclipses of up to 92 minutes and Mars aphelion power generation capability of less than 500W this generates a perpetual trade-off between support for the 65W X-band transmitter and science instrument operations. This paper seeks to examine the relationship between the mission operations concept and the operational flexibility that has been required to meet (and largely exceed) the mission objectives within the new envelope of constraints (power, downlink, fuel) and opportunities (additional ground stations, resources etc). The flexibilities provided by the original operations concept are identified and discussion is made of how these have been “stretched” to cope with the evolving mi ssion. Several aspects of the mission concept have been modified in light of flight experience. One significant change was the move from a “coverage” (mapping) science mission to a “target & coverage” science concept, based on improved knowledge of the mission's capabilities and on scientific opportunities foreseen by the science teams. Paradoxically this shift occurred at a time when the availability of three ground stations started to allow a full coverage over the nominal mission. Why these modifications have been made and the impact on the mission both in terms of cost and mission objectives is also discussed. The success of the Mars Express mission is largely to the flexibility provided by the original mission operations concept. This flexibility was partly enforced by the physics of Mars’ orbital missions (significantly eccentric solar orbit and relative distance to Earth ensuring significant variation on both power and data-downlink capabilities over the nominal mission), and partly due to rigorous and complex constraint checking at missionplanning level. Significant lessons can be learned from Mars Express in this respect; it is important to understand for any mission how the flexibilities provided by the operations concept could be used to cope with changes in system-level margins due to failures, anomalies or changes in the mission requirements late in the design stage or even in flight.
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- (del) (cur) 16:14, 22 February 2007 . . Rusocer (Talk | contribs) . . 0×0 (238,043 bytes) (Mars Express, ESA's first mission to orbit another planet, was launched on 2 June 2003 and arrived at Mars on 25 December 2003. Since orbit insertion it has successfully imaged more than 45% of Mars in infra-red and visible spectrums at resolutions of 10-)
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