Preview

Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering

Advanced search

Design and development of Cartesian propulsion system of the autonomous docking module for target acquisition

https://doi.org/10.25206/2588-0373-2023-7-3-70-81

EDN: OGSFTS

Abstract

The concept of building an orbital complex for operational interception of a target is proposed, including in its composition the method of ballistic construction of operational interception, recommendations to the design appearance of the Cartesian propulsion system of the autonomous docking module, functioning at the stage of close-in guidance during tether delivery from the upper stage to the target, at the stage of capture and transfer of the target to the disposal orbit as part of the rotating tether space system. As a criterion for selecting the Cartesian propulsion system design (fuel reserves, thrust of each chamber and their number, minimum change in the coordinates of the autonomous docking module center of mass over the entire interval of Cartesian propulsion system operation), the minimum mass of the autonomous docking module is taken. For comparison, two methods of constructing the ballistic scheme of target intercept are considered: the classical method, with the orbital complex entering the target orbit with zero relative velocities, and the method based on the use of rotating tether space system, with the orbital complex entering the target intercept orbit with velocities at the rendezvous point of up to 200 m/s.

About the Authors

V. I. Trushlyakov
Omsk State Technical University
Russian Federation

Trushlyakov Valeriy Ivanovich, Doctor of Technical Sciences, Professor of Aircraft and Rocket Building Department

AuthorID (RSCI): 9914

AuthorID (SCOPUS): 35792803600

ResearcherID: D-7270-2015

Omsk, Prospect Mira, 11, 644050



V. V. Yudintsev
Omsk State Technical University
Russian Federation

Yudintsev Vadim Vyacheslavovich, Candidate of Technical Sciences, Assistant Professor, Senior Researcher at the Research Laboratory «Steam and Gas Mixtures in Launch Vehicle Designs»

AuthorID (SCOPUS): 36676070000 ResearcherID: N-1367-2014

Omsk, Prospect Mira, 11, 644050



V. A. Urbansky
Omsk State Technical University
Russian Federation

Urbansky Vladislav Alexandrovich, Graduate Student of Aircraft and Rocket Building Department

AuthorID (RSCI): 978934

ResearcherID: AAX-1703-2021

Omsk, Prospect Mira, 11, 644050



S. Yu. Onishchuk
Omsk State Technical University
Russian Federation

Onishchuk Sergei Yurievich, Graduate Student of Aircraft and Rocket Building Department

AuthorID (RSCI): 979474

AuthorID (SCOPUS): 57211128570

ResearcherID: D-9183-2019

Omsk, Prospect Mira, 11, 644050



D. A. Klenin
Omsk State Technical University
Russian Federation

Klenin Danila Andreyevich, Laboratory Assistant at the Research Laboratory «Steam and Gas Mixtures in Launch Vehicle Designs»

AuthorID (RSCI): 1210637

Omsk, Prospect Mira, 11, 644050



References

1. Kessler D. J., Cour-Palais B. G. Collision frequency of artificial satellites: The creation of a debris belt // Journal of Geophysical Research: Space Physics. 1978. Vol. 83, no. A6. P. 2637–2646. DOI: 10.1029/JA083iA06p02637. (In Engl.).

2. Schaub H., Jasper L. E. Z., Anderson P. V. [et al.]. Cost and risk assessment for spacecraft operation decisions caused by the space debris environment // Acta Astronautica. 2015. Vol. 113. P. 66–79. DOI: 10.1016/j.actaastro.2015.03.028. (In Engl.).

3. Trushlyakov V. I., Yudintsev V. V., Urbansky V. A. [et al.]. Analiz sostoyaniya razrabotok sredstv ochistki orbit v okolozemnom kosmicheskom prostranstve ot ob”yektov krupnogabaritnogo kosmicheskogo musora [The analysis of the state of development of devices for cleaning orbits in near-Earth space from large-sized space debris objects] // Omskiy nauchnyy vestnik. Ser. Aviatsionno-raketnoye i energeticheskoye mashinostroyeniye. Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering. 2022. Vol. 6, no. 4. P. 42–52. DOI: 10.25206/2588-0373-2022-6-4-42-52. EDN: EETJHM. (In Russ.).

4. Tekhnicheskiye kharakteristiki transportnogo gruzovogo korablya «Progress MS». RKK «Energiya» im. S.P. Koroleva. [Technical characteristics of the Progress MS transport cargo spacecraft. RSC Energia named after S. P. Korolev]. URL: https://www.energia.ru/ru/spaceactivities/progress-ms/specifications.html (accessed: 07.08.2023). (In Russ.).

5. Trushlyakov V. I., Yudintsev V. V. Rotary Space Tether System for Active Debris Removal // Journal of Guidance, Control, and Dynamics. 2020. Vol. 43, no. 2. P. 354–364. DOI: 10.2514/1.G004615. (In Engl.).

6. Trushlyakov V. I., Yudintsev V. V. Dynamics of rotating tethered system for active debris removal // Acta Astronautica. 2022. Vol. 195. P. 405–415. DOI: 10.1016/j.actaastro.2022.03.023. (In Engl.).

7. Anselmo L., Pardini C. Ranking upper stages in low Earth orbit for active removal // Acta Astronaut. 2016. Vol. 122. P. 19–27. DOI: 10.1016/j.actaastro.2016.01.019. (In Engl.).

8. Tsentr Khrunicheva i NITs RKP. Uspeshnyye ognevyye stendovyye ispytaniya agregatnogo modulya rakety-nositelya «Angara». [Khrunichev Center and SIC RKP. Successful firing bench tests of the aggregate module of the Angara launch vehicle]. URL: https://www.roscosmos.ru/24356/ (accessed: 19.08.2023). (In Russ.).

9. «Orël» – novyy KK Rossii. [«Oryol» – Russia's new spacecraft]. URL: https://habr.com/ru/companies/first/articles/684124/ (accessed: 19.08.2023). (In Russ.).

10. Sikharulidze Yu. G. Ballistika i navedeniye letatel’nykh apparatov [Ballistics and guidance of aircraft]. Moscow, 2014. 407 p. ISBN 978-5-9963-0531-5. (In Russ.).

11. Trushlyakov V. I., Yudintsev V. V. Method of Active Debris Removal Using Rotating Space Tether System // First Int'l. Orbital Debris Conf., December 2019. URL: https://www.hou.usra.edu/meetings/orbitaldebris2019/orbital2019paper/pdf/6167.pdf (accessed: 19.08.2023). (In Engl.).

12. Burdaev М. N. O poiske novykh metodov i form resheniya uravneniya Lamberta–Eylera [About finding new methods and forms of solving the Euler-Lambert equation] // Programmnyye Sistemy: Teoriya i Prilozheniya. Program Systems: Theory and Applications. Vol. 9, no. 4 (39). P. 293–305. DOI: 10.25209/2079-3316-2018-9-4-293-305. (In Russ.).

13. Nosseir A. E. S., Cervone A., Pasini A. Review of State-of-the-Art Green Monopropellants: For Propulsion Systems Analysts and Designers // Aerospace. 2021. Vol. 8, no. 1. 20 р. DOI: 10.3390/aerospace8010020. (In Engl.).

14. Cassese S., Gallo G., Mungiguerra S. [et al.]. Preliminary Design And Study of 5N HTP Monopropellant Thruster for Small Satellites // Acta Astronautica. 2022. Vol. 202. P. 94–103. DOI: 10.1016/j.actaastro.2022.10.006. (In Engl.).

15. Guseinov S. L., Fedorov S. G., Kosykh V. A. [et al.]. Katalizatory razlozheniya peroksida vodoroda, ispol’zuyemyye v raketnykh dvigatelyakh [Hydrogen peroxide decomposition catalysts used in rocket engines] // Zhurnal Prikladnoy Khimii. Russian Journal of Applied Chemistry. 2020. Vol. 93, no. 4. P. 467–487. DOI: 10.31857/S0044461820040015. EDN: AAFAOK. (In Russ.).


Review

For citations:


Trushlyakov V.I., Yudintsev V.V., Urbansky V.A., Onishchuk S.Yu., Klenin D.A. Design and development of Cartesian propulsion system of the autonomous docking module for target acquisition. Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering. 2023;7(3):70-81. (In Russ.) https://doi.org/10.25206/2588-0373-2023-7-3-70-81. EDN: OGSFTS

Views: 102

JATS XML


Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 License.


ISSN 2588-0373 (Print)
ISSN 2587-764X (Online)