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40:(acronym for Reconfigurable Platform for Observation, Telecommunications and Scientific Uses) is a 3-axis stabilized platform designed for mini-satellites weighing approximately 500 kg operating in low Earth orbit. The platform is used by six scientific satellites developed as part of the space program of the
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operation in low orbits as platforms for various science and applications. After an industrial consultation with the national prime contractors of the time, Aérospatiale (Cannes) was selected, in May 1996, as industrial prime contractor, with the system to be built in the Cannes-Mandelieu space center.
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The PROTEUS platform and command and control segment has been developed based on a partnership between CNES and Aérospatiale (now Thales). The integrated team carries out the design of the PROTEUS multi-mission bus, the industrial production of the platform and associated satellites of which is the
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Attitude control: the satellite is stabilized on 3 axes with a pointing precision of 0.15° (Jason-3). The fine sensors used to determine the orientation of the satellite are two three-axis star finder and three two-axis gyrometers. The coarse sensors are three-axis magnetometers and 8 solar sensors
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In 1993, CNES decided to launch the development of the PROTEUS mini-satellite program in parallel and jointly with the Jason-1 satellite, the first user for the platform. Program goals including meeting recurring requirements for satellite solutions in the 500 kg-700 kg class intended for
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PROTEUS is a 3-axis stabilized platform designed for missions in low earth orbit for satellites with a total mass of approximately 500 kg, including 270 kg for the platform excluding propellants. Its main features are as follows:
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By 2010, the PROTEUS platform accumulated 20 years of on-orbit success, with the five satellites that had been orbited: Jason-1, CALIPSO, CoRoT, Jason-2, and SMOS.
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Propulsion: liquid propellant rocket motors burning hydrazine with a Delta-v capacity of about 120 m/s. The mass of hydrazine carried is 28 kg (Jason-3).
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In the same multi-mission platform perspective, the
Myriade program to support mission objectives achievable with microsatellites weighing less than 200 kg.
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Energy: solar panels with an area of 9.5 m, with one degree of freedom and providing 450 watts (Jason-1) to 550 watts (Jason-3) at the theoretical end of life
194:, copy of Jason-2, ordered on February 24, 2010 by EUMETSAT and placed in orbit in January 2016. This is the most recent satellite using this platform.
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for measuring the height of the oceans, launched on
December 7, 2001. It celebrated its tenth anniversary in 2011 and reached end of mission in 2013
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responsibility of Thales Alenia Space. In accordance with the partnership agreements, CNES remains in contro of workfor its own missions.
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with an optical field of 4 ft. The orientation is corrected using four reaction wheels which are desaturated using magneto-couplers.
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Spacecraft
Guidance, Navigation and Control Systems, Proceedings of the 3rd ESA International Conference
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236:"JASON-1 (NASA-JPL/CNES) : A Successful Operational Story Throughout Hardware Ageing"
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Communications: S-band telecommunications with a maximum throughput of 800 kilobits/s.
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Data storage: 500 megabits for telemetry data and 2 gigabits for scientific data.
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Lifespan: 3 years for consumables, 5 years for hardware and radiation tolerance.
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540:"Attitude and Orbit Control System for Multimission Spacecraft Platform"
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488:"European SMOS and Proba-2 Successfully Launched by Rockot"
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182:, follow-on mission to Jason-1, launched on June 20, 2008.
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64:. The platform is developed by the satellite division of
398:"Calipso Observation Satellite Celebrates Anniversary!"
376:"Long-Running Jason-1 Ocean Satellite Takes Final Bow"
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Dimensions: 954 mm x 954 mm x 1,000 mm
301:"Myriade - The French microsatellite buses family"
279:"20 Years in Orbit for the PROTEUS Satellite Bus"
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234:Canton, Rémi; Pélipenko, Pierre (May 9, 2014).
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352:Bourguignon, Anne Marie (December 13, 2011).
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84:CALIPSO satellite (artist's rendering), 2005
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30:For the natural satellite of Neptune, see
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149:Artists rendering Jason-1 in orbit, 2007
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42:National Center for Space Studies (CNES)
27:Satellite platform built by Thales Group
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419:Carlisle, Camille M. (June 25, 2013).
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538:Sghedoni, M.; et al. (1997),
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467:. CNES. February 8, 2022
445:. eoPortal. May 30, 2012
281:. CNES. October 7, 2010
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423:. Sky & Telescope
215:. CNES. March 7, 2017
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46:European Space Agency
610:Satellites of France
421:"COROT Mission Ends"
303:. CNES. May 31, 2017
580:Thales Alenia Space
556:1997ESASP.381..133S
378:. JPL. July 3, 2013
248:10.2514/6.2014-1609
70:Thales Alenia Space
18:Proteus (Satellite)
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550:: 133–139,
519:December 2,
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382:December 2,
360:December 2,
337:December 2,
307:December 2,
285:December 2,
263:December 2,
219:December 2,
52:, 2 and 3,
589:Categories
565:9290922079
492:Space News
199:References
513:"Jason-3"
443:"Jason-2"
356:. ToulEco
327:EO Portal
323:"Jason-1"
213:"PROTEUS"
68:(in 2016
44:for the
552:Bibcode
192:Jason-3
168:CALIPSO
158:Jason-1
76:History
54:CALIPSO
50:Jason-1
38:PROTEUS
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465:"SMOS"
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60:, and
515:. JPL
174:CoRoT
58:CoRoT
560:ISBN
521:2022
499:2022
473:2022
451:2022
429:2022
406:2022
384:2022
362:2022
339:2022
309:2022
287:2022
265:2022
252:ISBN
221:2022
186:SMOS
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