Научная электронная библиотека ULRICH'S Periodicals Directory

Сибирский государственный университет
науки и технологий имени академика М.Ф. Решетнева

Сибирский аэрокосмический журнал
ISSN 2712-8970 (Print) ISSN 2782-5760 (on-line)

Сведения об образовательной организации

UDK UDC 629.7.015.4 Doi: 10.31772/2587-6066-2018-19-4-637-643
THE ANALYSIS OF THE IMPACT OF THE METHOD OF FASTENING ON STRAIN-STRESS BEHAVIOR OF COMPOSITE OVERWRAPPED PRESSURE VESSEL
E. D. Mironenko, A. E. Miheev
JSC Academician M. F. Reshetnev Information Satellite Systems, 52, Lenin Str., Zheleznogorsk, Krasnoyarsk region, 662972, Russian Federation; Reshetnev Siberian State University of Science and Technology, 31, Krasnoyarsky Rabochy Av., Krasnoyarsk, 660037, Russian Federation
Currently, composite overwrapped pressure vessels (COPV), with high weight efficiency, are widely used in spacecraft (SC). In satellite construction COPVs provide necessary volume of working fluid for the realization of a highly efficient scheme of raising SC into geostationary orbit using standard electric propulsion engines. The issue of using such vessels in order to increase the period of active lifetime of SC and the implementation of deep-space exploration programs is relevant as well. The urgent task is to ensure the reliability of COPVs. The study of foreign literature suggests that fastening elements in direct contact with the vessel, have an important impact on the strain-stress behavior (SSB) of the vessel. The paper discusses the basic methods of fastening large-sized COPVs having a spherical shape – an adapter module is made in the form of a “skirt” and a cable-stayed system. We have created a finite element model (FEM) of COPV to analyze the effect of fastening elements on SSB of COPV. The analysis of the obtained results of the calculation shows that a cable-stayed system has almost no effect on SSB of COPV, in contrast to a composite “skirt”, which reduces the effective stresses in the place of attachment to the vessel by two times or more, causing uneven distribution of stresses. The composite “skirt” directly transfers its buckling mode to the vessel, which reflects the significant effect of the “skirt” on the vessel’s SSB. The use of a composite “skirt” in comparison with a cable-stayed system has high probability of COPV failure. The obtained results show that a cable-stayed system is more effective way to fasten COPV than a composite “skirt”.
Keywords: composite overwrapped pressure vessel, strain-stress behavior, cable-stayed system, spacecraft.
References

1. Mironenko E. D., Kravchenko I. A., Babichev A. A. [Development and implementation in industrial production of composite anisogrid power structures, high pressure xenon tank and their interfaces in order to increase the efficiency of telecommunication spacecraft]. Nadezhda Rossii. 2016, No. 2, P. 9–14 (In Russ.).

2. Kosenko V. E., Akimov A. N., Vygonskiy Yu. G. Razrabotka i vnedrenie v promyshlennoe proizvodstvo unifitsirovannoy vysokoehnergeticheskoy kosmicheskoy platformy «EHkspress-2000» i sozdanie na ee baze sovremennykh, konkurentosposobnykh kosmicheskikh apparatov svyazi i telekommunikatsiy [Development and implementation of a unified high-energy space platform “Express-2000” in industrial production and the creation of modern, competitive communications and telecommunications spacecraft. Description of work]. AO ISS, 2015, 100 p. (In Russ.).

3. Babanov A. A, Vnukov A. A., Doronkin M. N. Sposob vyvedeniya kosmicheskogo apparata na geostatsionarnuyu orbitu s ispol’zovaniem dvigateley maloy tyagi [The method of launching spacecraft into a geostationary orbit using thrusters]. Patent RF, No. 2586945, 2014, 10 p.

4. Borodin L. M., Ovechkin G. I., Gordeev A. V. Bak vysokogo davleniya [High pressure tank]. Patent RF No.2589956, 2013, 8 p.

5. Mironenko E. D. [On the issue of fixing high pressure metal composite tanks]. 8-y Vserossiyskiy molodyozhnyy konkurs nauchno-tekhnicheskikh rabot i proektov «Molodyozh’i budushchee aviatsii i kosmonavtiki». Annotatsii konkursnykh rabot [8th All-Russian Youth Competition for Scientific and Technical Works and Projects “Youth and the Future of Aviation and Cosmonautics”. Annotations of entries]. MAI, 2016, P. 252–253 (In Russ.).

6. Vasil’ev V. V., Razin A. F., Sin’kovskiy F. K. [Optimal shape of a composite pressure cylinder with a metal liner]. Kompozity i nanostruktury. 2014, No. 1, P. 2–8 (In Russ.).

7. Kravchenko I. A., Mikheev A. V., Borodin L. M. [Features of the use of metal composite tanks on board spacecraft]. Materialy XVII Mezhdunar. nauch. konf. Reshetnevskie chteniya [Proceedings of the XVII Intern. scientific conf. Reshetnev Readings]. 2013, No. 1, P. 71–72 (In Russ.).

8. Azarov A. V., Babichev A. A., Sin’kovskiy F. K. [Design and manufacture of a composite high-pressure tank for spacecraft]. Kompozity i Nanostruktury. 2013, No 4, P. 44–57. (In Russ.).

9. Arkhipov Yu. S., Buldashev S. A., Dudin A. I. Opyt sozdaniya kompozitnykh emkostey dlya kosmicheskikh apparatov tipa Ekspress [The experience of creating composite containers for spacecraft Express] (InRuss.). Available at: http://niimashspace.ru/pdf/korol18190413.pdf (accessed: 06.11.2018).

10. Composite Pressure Vessel Data Sheet. Arde Part Number 4790. Available at: http://www.ardeinc.com/sketches/copv/4790.pdf (accessed: 06.11.2018).

11. Gardiner G. Space mission maximized via minimized survivability. High-Performance Composites. 2013, Vol. 21, No. 2, P. 62–64.

12. Radtke W., Scharringhausen J., Windisch M. Alphabus Propellant Tank: Manufacturing, NDI and Damage Control. 3rd IAASS International Space Safety Conference COPV Safety and Integrity Workshop, Italy, 2008, 24 p.

13. Composite Pressure Vessel Data Sheet. Model PTP-1910. 2018. Available at: http://www.mt-aerospace.de/files/mta/tankkatalog/Datenblatt_PTP-1910_Heritage-notforsale.pdf (accessed: 06.11.2018).

14. Randolph T. M. [Qualification of Commercial Electric Propulsion Systems for Deep Space Missions]. 30th International Electric Propulsion Conference. Italy, 2007, 16 p.

15. Robert H. Estes, James Harris, N. R. Moore. [Summary of the Development of a Demiseable Composite Overwrapped Hydrazine Tank for the Global Precipitation Measurement Mission from Concept to Delivery]. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Georgia, 2012, 68 p.


Mironenko Evgeny Dmitrievich – product design engineer, JSC “Academician M. F. Reshetnev “Information

Satellite Systems”. E-mail: mironenko91@iss-reshetnev.ru.

Miheev Anatoly Egorovich – Dr. Sc., professor, head of Department, Reshetnev Siberian State University

of Science and Technology. E-mail: michla@mail.ru.


  THE ANALYSIS OF THE IMPACT OF THE METHOD OF FASTENING ON STRAIN-STRESS BEHAVIOR OF COMPOSITE OVERWRAPPED PRESSURE VESSEL