Phobos-Grunt: Russian sample return mission

Marov, M. Ya.; Avduevsky, V. S.; Akim, E. L.; Éneev, T. M.; Kremnev, R. S.; Kulikov, S. D.; Pichkhadze, K. M.; Popov, G.A.; Rogovsky, G.N.

doi:10.1016/s0273-1177(03)00515-5

Cited by 58 publications

(22 citation statements)

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“…Это предложе-ние рассматривалось на волне развития российско-американского сотрудниче-ства по космосу по совместной программе «вместе к марсу», однако этот проект не был поддержан. Затем подобные предложения обсуждались еще на несколь-ких конференциях и в публикациях, в частности [Galeev et al, 1996;Zakharov, 1998;Zakharov, Sukhanov, 1999;Avduevsky et al, 1999;Авдуевский и др., 2000;Marov et al,2004]. Наша страна пыталась реализовать амбициозный проект исследований марса в 1996 г.…”

Section: генеральный конструктор и генеральный директор нпо им са unclassified

“…Главная задача проекта ФОбОС-ГРУНт -доставка на Землю вещества спутни-ка марса Фобоса, для его изучения в лабораториях [Галимов, 2009;Marov et al, 2004;Galeev et al, 1996]. Это предполагает посадку космического аппарата на Фобос, забор образцов в пределах доступности манипулятора грунтозаборного устройства, загрузку их в возвращаемую капсулу и доставку ее на Землю.…”

Section: га самков ан белкин ав лемцева нпо им са лавочкинаunclassified

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About the cause of the emergency situation with the Russian spacecraft "Phobos-Grunt"

Кудрявцева¹

2016

EJSI

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Section: генеральный конструктор и генеральный директор нпо им са unclassified

Section: га самков ан белкин ав лемцева нпо им са лавочкинаunclassified

About the cause of the emergency situation with the Russian spacecraft "Phobos-Grunt"

Кудрявцева¹

2016

EJSI

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“…The question of water ice inside Phobos was addressed by Fanale and Salvail (1990). (Zakharov, 2002;Marov et al, 2004). In addition there have been many Earth-based telescopic observations (e.g.…”

Section: Scientific Backgroundmentioning

confidence: 99%

“…• Phobos-Grunt ('Phobos-Soil') sample return (Zakharov, 2002;Marov et al, 2004). An 'engineering model' of the surface of Phobos has been generated in support of this mission Kuzmin and Zabuleva, 2003).…”

Section: In Recent Years Proposals For Future Missions To Phobos Andmentioning

confidence: 99%

Mars Phobos and Deimos Survey (M-PADS) – A martian Moons orbiter and Phobos lander

Ball

Price

Walker

et al. 2009

Advances in Space Research

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We describe a Mars 'Micro Mission' for detailed study of the martian satellites Phobos and Deimos. The mission involves two ~330 kg spacecraft equipped with solar electric propulsion to reach Mars orbit. The two spacecraft are stacked for launch: an orbiter for remote investigation of the moons and in situ studies of their environment in Mars orbit, and another carrying a lander for in situ measurements on the surface of Phobos (or alternatively Deimos). Phobos and Deimos remain only partially studied, and Deimos less well than Phobos. Mars has almost always been the primary mission objective, while the more dedicated Phobos project (1988-89) failed to realise its full potential. Many questions remain concerning the moons' origins, evolution, physical nature and composition. Current missions, such as Mars Express, are extending our knowledge of Phobos in some areas but largely neglect Deimos. The objectives of M-PADS focus on: origins and evolution, interactions with Mars, volatiles and interiors, surface features, and differences. The consequent measurement requirements imply both landed and remote sensing payloads. M-PADS is expected to accommodate a 60 kg orbital payload and a 16 kg lander payload. M-PADS resulted from a BNSC-funded study carried out in 2003 to define candidate Mars Micro Mission concepts for ESA's Aurora programme.

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“…23) Russia carried out the Phobos-Grunt Sample Return Mission, which was planned to orbit Phobos to explore it, obtain a sample and then return with the sample. 24) However, the Phobos-Grunt mission ended in failure because of a launch vehicle problem, along with the Yinghuo-1.…”

Section: Introductionmentioning

confidence: 99%

Deimos Encounter Trajectory Design for Piggyback Spacecraft Launched for Martian Surface Reconnaissance

Wang

2015

Trans. Japan Soc. Aero. S Sci.

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This paper discusses a trajectory design for imaging both Mars and Deimos, which meets the requirements of the next Chinese mission to Mars and Deimos. Compared to Viking-1, being weak in systematic schedules in its original and extended missions, which resulted in the use of more fuel and reducing encounter opportunities, a multipurpose design is addressed in this paper for imaging both Mars and Deimos at Pre-Phase A, not after launch. A frozen and repeating orbit is employed to provide as many as 280 periodic encounters within 100 km of Deimos, in contrast to the fly-around mode used by Phobos-1/2 and Phobos-Grunt, requiring much fuel to guide the spacecraft to the vicinity of Phobos from the highly elliptical captured orbit. To enable encounters with Deimos under all of the perturbations and orbital control and determination errors, the station-keeping strategies for the arguments of periareon and latitude are implemented by some corrections to the semi-major axis and inclination, respectively. A numerical simulation is used to verify the encounter opportunities with the help of the station-keeping strategies. Detailed investigations on imaging, lighting and access conditions show that a working orbit is beneficial for imaging both the Martian surface and Deimos. Therefore, it is concluded that designing the trajectory of the piggyback spacecraft to be carried by the main orbiter in the next Chinese Mars mission during Pre-Phase A is practical from the engineering perspective.

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Phobos-Grunt: Russian sample return mission

Cited by 58 publications

References 1 publication

About the cause of the emergency situation with the Russian spacecraft "Phobos-Grunt"

About the cause of the emergency situation with the Russian spacecraft "Phobos-Grunt"

Mars Phobos and Deimos Survey (M-PADS) – A martian Moons orbiter and Phobos lander

Deimos Encounter Trajectory Design for Piggyback Spacecraft Launched for Martian Surface Reconnaissance

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