Development of the propulsion construction and the trajectory of the spacecrafts for the study of Martian planetary system
Автор: I. V. Platov, A. V. Simonov, A. L. Vorobyev, E. S. Gordienko
Журнал: Siberian Aerospace Journal @vestnik-sibsau-en
Рубрика: Aviation and spacecraft engineering
Статья в выпуске: 3 vol.20, 2019 года.
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The article provides a brief description of the flight scheme of a prospective automatic spacecraft intended for the study of Mars and its satellites by remote and contact methods. At the near-Martian expedition site, it is planned to first bring the vehicle into orbit of the artificial satellite Deimos, and then landing on Phobos with the subsequent delivery of its soil to Earth. The main ballistic characteristics of the spacecraft flight conditions at all stages of the flight at launch after 2025 are given. The time frames for the five starting periods are considered - in 2026, 2028, 2030, 2033 and 2035. The launch of the spacecraft on the flight path to Mars is performed by a heavy class launcher. The article describes the design of the vehicle, propulsion systems of its modules and flight scheme at all stages – from launch from the Earth to landing on Phobos, and returning back to Earth. The article describes the propulsion systems of the main spacecraft units proposed for the mission implementation – the propulsion module, the flight landing platform and the return vehicle. The designs of these units are provided in the work. Flight schemes have been developed in accordance with their characteristics, which allows conducting remote study of Deimos, making a soft landing on the surface of Phobos, and then delivering samples of its soil to Earth. The project should be developed on the basis of the spacecraft launch from the Vostochny launch site by the Angara- A5 launch vehicle and the KVTK upper stage. An alternative variant of the construction of a spacecraft involves the use of a vehicle of a lighter class - perspective Soyuz-5 launch vehicle and Fregat-SBU upper stage. In this case, the engine module is excluded, and the flight and landing module is replaced by a heavier version with larger tanks. Both proposed options for constructing a spacecraft make it possible to implement the developed trajectory, while ensuring full-time operation of the target equipment and conducting a set of experiments during a given period of active spacecraft existence.
Spacecraft, propulsion system, trajectory, flight scheme, interplanetary transfer, Mars, Phobos, Deimos.
Короткий адрес: https://sciup.org/148321695
IDR: 148321695 | DOI: 10.31772/2587-6066-2019-20-3-356-365
Список литературы Development of the propulsion construction and the trajectory of the spacecrafts for the study of Martian planetary system
- Khartov V. V. [From research to development of resources of the moon. Yesterday and tomorrow (the 50th anniversary of the space activities of the NPO named after S. A. Lavochkin)]. Vestnik NPO imeni S. A. Lavochkina. 2015, No. 3 (29), P. 8–13 (In Russ.).
- Efanov V. V. et all. [Lavochkin Association aircrafts (to the 80th anniversary of the enterprise)]. Vestnik NPO imeni S. A. Lavochkina. 2017, No. 2 (36), P. 5–16 (In Russ.).
- Asyushkin V. A. Vikulenkov V. P., Ishin S. V. [Outcome of development and operation initial phases of versatile space tugs of Fregat]. Vestnik NPO imeni S. A. Lavochkina. 2014, No. 1, P. 3–9 (In Russ.).
- Birukov A. S., Makarov V. P., Markachev N. A. et al. [Special features of structural layouts and experimental verification of Fregat versatile space tug and transfer compartments]. Vestnik NPO imeni S. A. Lavochkina. 2014, No. 1, P. 26–36 (In Russ.)
- Efanov V. V., Matrynov M. B., Pichkhadze K. M. [Space robots for science researches]. Sciense in Russia. 2012, No. 2, P. 4–14 (In Russ.).
- Polishchuk G. М., Pichkhadze К. М., Efanov V. V., Martynov М. B. [Space modules of Phobos-Grunt space complex for next-generation interplanetary stations]. Vestnik NPO imeni S. A. Lavochkina. 2009, No. 2, P. 3–7 (In Russ.).
- Asyushkin V. A. Vikulenkov V. P., Lebedev K. N., Lukyanets S. V., Moroz N. G. [Development of higheffective metal-base composite higt-pressure vessel]. Vestnik NPO imeni S. A. Lavochkina. 2015, No. 1, P. 19–27 (In Russ.).
- Akim E. L. et all. [Ballistics, navigation and spacecraft flight control in the Phobos-Grunt project]. Izvestiya RAN. Teoriya i systemi upravleniya. 2002, No. 5, P. 153–161 (In Russ.).
- Simonov A. V. et al. [Ballistic flight scheme of the spacecraft Phobos-Grunt]. Vestnik NPO imeni S. A. Lavochkina. 2011, No. 3(9), P. 66–73 (In Russ.).
- Morskoy I. M. et all. [Spacecraft’s flight scheme]. Fobos-grunt. Proekt kosmicheskoy ekspeditsii. 2011, Vol. 1, P. 58–73 (In Russ.).
- Borovin G. K. et al. [Devoted to continuous fruitful cooperation of S. A. Lavochkin NGO and M. V. Keldysh IPM of RAS in space exploration – more than half a century]. Vestnik NPO imeni S. A. Lavochkina. 2017, No. 2 (36), P. 67–74 (In Russ.).
- Borovin G. K. et al. Ballistiko-navigacionnoye obespecheniye poletov avtomaticheskih kosmicheskih apparatov k telam solnechnoy systemi [Ballistic and navigational support of flights of automatic spacecraft to the Solar System bodies]. Khimki, 2018 (In Russ.).
- Tuchin A. G. [Quasisynchronous orbits and their application for spacecraft approach to Phobos]. Kosmicheskiye issledovaniya. 2007, Vol. 45, No. 2, P. 144–149 (In Russ.).
- Tuchin A. G. [Design of quasi-synchronous orbits of the spacecraft around Phobos to solve the problem of landing on its surface]. Kosmicheskiye issledovaniya. 2008, Vol. 46, No. 6, P. 536–546 (In Russ.).
- Akim E. L. et al. [Ballistics, navigation and spacecraft motion control at the stage of its landing on the surface of Phobos]. Kosmicheskiye issledovaniya. 2009, Vol. 47, No. 4, P. 332–342 (In Russ.).
