طراحی سیستم جاذب ارتعاشات برای میراسازی ارتعاش وارده بر بلوک تأمین انرژی موشک‌های ماهواره‌بر

ملک زاده فرد, کرامت; شاهی, علیرضا; پورموید, علیرضا

doi:10.22034/jtae.2026.10.1.1

طراحی سیستم جاذب ارتعاشات برای میراسازی ارتعاش وارده بر بلوک تأمین انرژی موشک‌های ماهواره‌بر

نوع مقاله : علمی پژوهشی

نویسندگان

کرامت ملک زاده فرد ¹

علیرضا شاهی ²

علیرضا پورموید ³

¹ استاد، مجتمع دانشگاهی هوافضا، دانشگاه صنعتی مالک اشتر، تهران، ایران

² کارشناسی ارشد هوافضا، مجتمع دانشگاهی هوافضا، دانشگاه صنعتی مالک اشتر، تهران، ایران

³ دانشیار، دانشکده مهندسی مکانیک، دانشگاه پدافند هوایی خاتم‌الانبیاء (ص)، تهران، ایران

10.22034/jtae.2026.10.1.1

چکیده

بلوک‌های تأمین انرژی در طول انجام مأموریت پروازی خود، تحت اثر محیط‌های دینامیکی و ارتعاشی مختلفی از جمله ارتعاشات با ورودی سینوسی، پله قرار می‌گیرند که اثر آن‌ها، عمده‌ترین دلیل در تخریب و تضعیف عملکرد کلی موشک‌های حامل می‌باشد. از قسمت‌های مختلف موشک‌های ماهواره‌بر، زیرسیستم‌های الکترونیکی و بلوک تأمین انرژی موشک‌های ماهواره‌بر است که حساس به ارتعاشات ایجادی توسط موشک ماهواره‌بر می‌باشد. در این مقاله به تشریح استفاده از جاذب‌های نیمه فعال و جاذب ابتکاری پرداخته شده و برای اولین بار جهت میرا سازی ارتعاشات وارده بر سامانه‌های بلوک تأمین انرژی موشک‌های ماهواره‌بر بررسی شده‌است. به این طریق که برای تحلیل کلی بلوک تأمین انرژی معادله حرکت آن در فضای حالت به‌دست آمده است. در قدم بعدی باتوجه به نوع معادله حرکت سیستم به تحلیل ارتعاشات وارده بر ماهواره‌بر راه‌های میراسازی آن بررسی می‌شود. سیستم ابتکاری این پژوهش با استفاده از جاذب غیرفعال و در نهایت با استفاده از ترکیب جاذب‌های فعال و غیرفعال (پایه‌های الاستومری) به میرا سازی ارتعاشات ایجادی از زمان آماده به پرتاب، در حین پرتاب و در زمان پرواز پرداخته شده‌است. همچنین نتایج تحقیق نشان می‌دهد که سیستم میراگر ابتکاری مورداستفاده، راندمان را 18 درصد بیشتر نسبت به جاذب غیرفعال و 16 درصد بهتر از جاذب فعال می‌نماید که در نوع خود بسیار قابل‌توجه است.

کلیدواژه‌ها

ماهواره‌بر

بلوک تأمین انرژی

جاذب ارتعاشات

ایزولاتور

نیمه فعال

موضوعات

سازه‌/مکانیک جامدات/دینامیک جامدات/ارتعاشات/آئروالاستیسیته/...

عنوان مقاله English

Vibration Absorber System Design to Dampen Vibrations on the Block of Power Supply of Satellite Launch Vehicle

نویسندگان English

Keramat Malekzadeh Fard ¹

Alireza Shahi ²

Alireza Pourmoayed ³

¹ Faculty of Aerospace, Malek Ashtar University of Technology, Tehran, Iran

² Faculty of Aerospace, Malek Ashtar University of Technology, Tehran, Iran

³ Faculty of Mechanical Engineering, University of Khatamul-Anbiya Air Defense, Tehran, Iran

چکیده English

During flight missions, power supply blocks are subjected to various dynamic environments, including sinusoidal and step input vibrations, which are the primary causes of structural degradation and reduced performance of satellite launch vehicles. Among the components of these vehicles, electronic subsystems and power supply blocks are particularly susceptible to vibration-induced failures. This study investigates, for the first time, the application of semi-active absorbers in combination with a novel damping mechanism to reduce vibrations affecting the power supply block systems of satellite launch vehicles. To facilitate a comprehensive analysis, the motion equation of the power supply block was formulated in state-space representation. Based on the system's dynamic model, vibration responses were analyzed, and mitigation strategies were assessed. The proposed system incorporates a passive absorber and, ultimately, a hybrid configuration combining active and passive elements using elastomeric bases to suppress vibrations encountered during pre-launch, launch, and flight phases. Results demonstrate that the novel damper system improves efficiency by 18% compared to passive absorbers and by 16% relative to active absorbers, representing a substantial performance enhancement.

کلیدواژه‌ها English

Satellite

Power supply block

Vibration absorber

Isolator

Semi-active

[1] B. Blazejczyk-Okolewska, "Analysis of an impact damper of vibrations,"Chaos, Solitons and Fractals, vol. 12, no. 11, pp. 1983-1988, 2001, https://doi.org/10.1016/S0960-0779(00)00146-6.

[2] V. L. Shinde and A. K. Pathak, "Review on particle damping technique for vibration suppression," International Journal of Innovative Research in Science, Engineering And Technology, vol. 5, no. 3, pp. 2890-2895, 2016, https:// doi:10.15680/IJIRSET.2016.0503028.

[3] Z. Lu, Z. Wang, S. F. Masri, and X. Lu, "Particle impact dampers: Past, present, and future," Structural Control and Health Monitoring, vol. 25, no. 1, 2018, Art. no. e2058, https://doi.org/10.1002/stc.2058.

[4] S. M. Hasheminejad, A. H. Rabiee, and A. H. D. Markazi, "Dual-functional electromagnetic energy harvesting and vortex-induced vibration control of an elastically mounted circular cylinder," Journal of Engineering Mechanics, vol. 144, no. 3, 2018, Art. no. 04017184, https://doi.org/10.1061/(ASCE)EM.1943-7889.0001411.

[5] Y. Li, W. Shen, and H. Zhu, "Vibration mitigation of stay cables using electromagnetic inertial mass dampers: Full-scale experiment and analysis," Engineering Structures, vol. 200, 2019, Art. no. 109693, https://doi.org/10.1016/j.engstruct.2019.109693.

[6] D. J. Mead, "Passive vibration control," New York: John Wiley, 1998, https://lccn.loc.gov/98048784.

[7] J. Chen and C. T. Georgakis, "Tuned rolling-ball dampers for vibration control in wind turbines," Journal of Sound and Vibration, vol. 332, no. 21, pp. 5271-5282, 2013, https://doi.10.1016/j.jsv.2013.05.019.

[8] W. Xiao, Y. Huang, H. Jiang, H. Lin, and J. Li, "Energy dissipation mechanism and experiment of particle dampers for gear transmission under centrifugal loads," Particuology., vol. 27, pp. 40-50, 2016, https://doi.org/10.1016/j.partic.2015.10.007.

[9] L. Luo, D. Liu, Z. Jiang, and D.Cheng, "Research on the design and damping control of rocket maritime transportation device," In Journal of Physics: Conference Series, vol. 2775, no. 1, 2024, Art. no. 012023, https://doi.10.1088/1742-6596/2775/1/012023.

[10] W. Evans et al.," Welding of Crack Sensitive Aluminum Alloys for Liquid Rocket Propulsion Applications," In Worldwide Advanced Manufacturing Symposium, 2024,

[11] J. Wang, B. Wang, Z. Liu, H. Li, and C. Zhang, "Seismic response mitigation of building structures with a novel vibro-impact dual-mass damper," Engineering Structures, vol. 215, 2020, Art. no. 110673, https://doi.org/10.1016/j.engstruct.2020.110673.

[12] [Online]. Available: https://daily.sharif.ir/magazine.

[13] H. Safaeifar and A. Farshidianfar, "Experimental and analytical investigation of impact dampers in free vibration reduction with coulomb friction," Noise and Vibration Worldwide, vol. 5, no. 3, pp.91-103, 2022, https://doi.org/10.1177/09574565211055796.

[14] C. Poussot-Vassal, C. Spelta, O. Sename, S. M. Savaresi, and L. Dugard, "Survey on some automotive semi-active suspension control methods: A comparative study on a single-corner model," IFAC Proceedings, vol. 44, no. 1, pp. 1802-1807, 2011, https://doi.org/10.3182/20110828-6-IT-1002.00446.

[15] H. Wenzhi, Z. Hao, H. Wei, and Z. Zhiguo, "Design optimization of a low-cost three-stage launch vehicle with modular hybrid rocket motors," in Journal of Physics: Conference Series, vol. 2764, no. 1, 2024, Art. no. 012026, https://doi.10.1088/1742-6596/2764/1/012026.

[16] J. Singh, A. Srivastava, A. Gupta, R. Kumar, J. Rajput, and S. Ravichandran, "Inspection on Solid Fuel Propellant in Rocket Efficiency," Journal of Advanced Research in Applied Physics and Applications, vol. 7, no. 1, pp. 1-6, 2024, https://orcid.org/0009-0008-7701-8272.

[17] M. Nejati and S.Shokrollahi, "Dynamic response analysis of a nanosatellite in time and frequency domain due to the seperation," Aerospace Knowledge and Technology Journal, vol. 1, no. 2, pp. 33-42, 2013.

[18] J. Wang, B. Wang, Z. Liu, H. Li, and C. Zhang, "Seismic response mitigation of building structures with a novel vibro-impact dual-mass damper," Engineering Structures, vol. 215, 2020, Art. no. 110673, https://doi.org/10.1016/j.engstruct.2020.110673.

[19] S. Vekilov, V. Lipovskyi, and R. Pustovyi, "The problem of combustion instability in liquid rocket engines," Challenges and Issues of Modern Science, vol. 2, pp. 100-110, 2024.

[20] A. Das, A. Dutta, and S. K. Deb, "Performance of fiber‐reinforced elastomeric base isolators under cyclic excitation," Structural Control and Health Monitoring, vol. 22, no. 2, pp. 197-220, 2015, https://doi.org/10.1002/stc.1668.

[21] I. Alimjonov, "Technical malfunctions in the international space station's energy system and their solutions," Educational Research in Universal Sciences, vol. 44, no. 4, pp. 47-55, 2025, https://doi.org/10.5281/zenodo.14947013.

[22] M. R. Najafi and A. Motalebi, "A review of the performance parameters of magnetorheological vibration dampers," Journal of Vibration and Sound, vol. 12, no. 24, pp. 86-105, 2024.

[23] L. Auersch, "Soil–structure interaction and damping by the soil-effects of foundation groups, foundation flexibilitysoil stiffness and layers," Vibration, vol. 8, no. 5, pp. 1-28‏, 2025, https://doi. 10.3390/vibration8010005.

[24] H. R. Askarpour, A. Mazidi, and M. Rafeeyan, "Aeolian vibration analysis of transmission lines with spacers," Journal of Engineering Mechanic, vol. 32, no. 5, pp. 60-71‏, 2024.