A tether system at the L1, L2 collinear libration points of the mars-phobos system
DOI: 10.34759/trd-2022-122-02
Аuthors
*, **Samara National Research University named after Academician S.P. Korolev, 34, Moskovskoye shosse, Samara, 443086, Russia
*e-mail: aslanov_vs@mail.ru
**e-mail: neryadovskayadv@yandex.ru
Abstract
The article considers one of the L1 or L2 collinear libration points application for a tether system deployment in the direction of Phobos in a plane circular restricted three-body problem in the Mars-Phobos system. An orbital spacecraft by which one of the tether ends is being fixed is located in L1 or L2 collinear libration points and is being held in one of these unstable points by the low thrust of its engines. The equation of the tether system motion in the polar coordinates system was obtained for the tether of constant length, the equilibrium positions were found, and the dependence of the vibrations period on the tether length was determined. Comparison of approximate solution for the small angles of the tether deviation from the local vertical with the numerical one was performed. The article demonstrates that the system “fixed” either in both the L1 point and L2 has potential wells in cases when the tether is being directed towards the Phobos side. It was revealed that the dependencies of the vibrations period on the tether length for the L1 and L2 points were fundamentally different. Comparison for both L1 and L2 of approximate and numerical solutions revealed herewith that the vibrations amplitude remained constant in contrast to the frequency. The results of this study may be employed for the future space missions provision. Thus, for example, a space lift may be arranged in the Mars-Phobos system, which tether will pass through the L1 or L2 libraion point. Besides, such lift may serve as an intermediate station for conducting studies associated with the space exploration around it, as well as a platform for the interplanetary flights. “Fixing” the tether system in the L1 or L2collinear libration point of the Mars-Phobos system will allow conducting remote studies of Phobos employing a vehicle with sensors, which will hover above its surface.
Keywords:
tether system, libration point, state of equilibrium, phase plane, analytic solution, elliptic functionReferences
-
Danchenko O.M. Trudy MAI. 2012. № 59. URL: http://trudymai.ru/eng/published.php?ID=34404
-
Kochetkov A.A., Kurmazenko E.A., Khabarovskii N.N., Kamaletdinova G.R. Trudy MAI, 2011, no. 43. URL: http://trudymai.ru/eng/published.php?ID=24756
-
Sinitsyn A.A. Trudy MAI, 2017, no. 94. URL: http://trudymai.ru/eng/published.php?ID=80987
-
Ryazanov V.V. Trudy MAI, 2019, no. 107. URL: http://trudymai.ru/eng/published.php?ID=107837
-
Konstantinov M.S., Leb Kh.V., Petukhov V.G., Popov G.A. Trudy MAI, 2011, no. 42. URL: http://trudymai.ru/eng/published.php?ID=24274
-
Deutsch A.N., Head J.W., Ramsley K.R. et al. Science exploration architecture for Phobos and Deimos: The role of Phobos and Deimos in the future exploration of Mars, Advances in Space Research, 2018, vol. 62, pp. 2174-2186. DOI:10.1016/J.ASR.2017.12.017
-
Murchie S.L., Britt D.T., Pieters C.M. The value of Phobos sample return, Planetary and Space Science, 2014, vol. 102, pp. 176-182. DOI:10.1016/j.pss.2014.04.014
-
Marov M.Ya., Avduevsky V.S., Akim E.L.et al. Phobos-Grunt: Russian sample return mission, Advances in Space Research, 2004, vol. 33, pp. 2276-2280. DOI:10.1016/S0273-1177(03)00515-5
-
Martynov M.B., Alexashkin S.N., Khamidullina N.M. et al. Planetary Protection Principels Used for Phobos-Grunt Mission, Solar System Research, 2011, vol. 45, pp. 593-596. DOI:10.1134/S0038094611070185
-
Martynov M.B. The design philosophy of the Phobos-Grunt space vehicle, Solar System Research, 2012, vol. 46, pp. 493-497. DOI:10.1134/S0038094612070179
-
Celik O., Baresi N., Ballouz R.-L., Ogawa K., Wada K., Kawakatsu Y. Ballistic deployment from quasi-satellite orbits around Phobos under realistic dynamical and surface environment constraints, Planetary and Space Science, 2019, vol. 178. DOI: 10.1016/j.pss.2019.06.010
-
Conte D., Spencer D.B. Mission analysis for Earth to Mars-Phobos distant Retrograde Orbits, Acta Astronautica, 2018, vol. 151, pp. 761-771. DOI:10.1016/j.actaastro.2018.06.049
-
Ferri A., Pelle S., Belluco M., Voirin T., Gelmi R. The exploration of PHOBOS: Design of a Sample Return mission, Advances in Space Research, 2018, vol. 62, pp. 2163-2173. DOI:10.1016/j.asr.2018.06.014
-
Usui T., Bajo K., Fujiya W. et al. The Importance of Phobos Sample Return for Understanding the Mars-Moon System, Space Science Reviews, 2020, vol. 216. DOI:10.1007/s11214-020-00668-9
-
Canalias E., Lorda L., Martin T., Laurent-Varin J., Marty J.C., Mimasu Y. Trajectory analysis for the Phobos proximity phase of the MMX mission, International Symposium on Space Flight Dynamics, 2017. URL: https://issfd.org/ISSFD_2017/paper/ISTS-2017-d-006__ISSFD-2017-006.pdf
-
Joffre E., Zamaro M., Silva N., Marcos A., Simplício P. Trajectory design and guidance for landing on Phobos, Acta Astronautica, 2018, vol. 151, pp. 389-400. DOI:10.1016/j.actaastro.2018.06.024
-
Kempton K., Pearson J., Levin E. et al. Phase 1 Study for the Phobos L1 Operational Tether Experiment (PHLOTE). End Report. NASA, 2018, 91 p. URL: https://ntrs.nasa.gov/api/citations/20190000916/downloads/20190000916.pdf
-
Aslanov V.S., Prospects of a tether system deployed at the L1 libration point, Nonlinear Dynamics, 2021, vol. 106. URL: https://doi.org/10.1007/s11071-021-06884-4
-
Markeev A.P. Tochki libratsii v nebesnoi mekhanike i kosmodinamike (Libration points in celestial mechanics and cosmodynamics), Moscow, Nauka, 1978, 312 p.
-
Zhuravskii A.M. Spravochnik po ellipticheskim funktsiyam (Handbook of Elliptic Functions), Moscow-Leningrad, AN SSSR, 1941, 235 p.
Download