Preprint / Version 1

Challenges of Hypersonic Travel

##article.authors##

  • Aryan Soma Riverside High School

DOI:

https://doi.org/10.58445/rars.1287

Keywords:

engineering, aircraft, speed

Abstract

Hypersonic travel has the potential to revolutionize aviation as it can drastically reduce travel time for long distances, making global and interstellar travel more efficient. When reaching hypersonic speeds without proper thermal protection systems (TPS), the aircraft’s interior could reach 3000 to 5000 degrees Fahrenheit, frying both any electrical systems and passengers on board. This paper will review essential design elements such as materials, heat management systems, and drag profiles, which will help manage the extreme heat within hypersonic vehicles. Materials are vital in reducing weight, increasing fuel efficiency, and resisting external heat, all of which are factors in improving TPS. Heat management systems are also crucial as aircrafts need to cool down the internal heat their engines produce. Making an aircraft design with as little drag as possible is essential for TPS  as it reduces heat caused by friction. This paper will identify challenges and future steps for TPS designs.

References

Glass, D. E. (2008). Ceramic matrix composite (CMC) thermal protection systems (TPS) and hot structures for hypersonic vehicles. 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. https://doi.org/10.2514/6.2008-2682

Gülhan, A. & German Aerospace Center (DLR). (2015). Challenges of Hypersonic Flight Health-Monitoring. In Workshop on Hypersonic Morphing (Hypmoces) [Conference-proceeding]. https://elib.dlr.de/101783/1/Challenges%20of%20Hypersonic%20Flight%20HM.pdf

Huang, J., & Yao, W. (2020). Active flow control by a novel combinational active thermal protection for hypersonic vehicles. Acta Astronautica, 170, 320–330. https://doi.org/10.1016/j.actaastro.2020.01.033

IATA. (2019, December). Global Outlook for Air Transport. https://www.iata.org/en/iata-repository/publications/economic-reports/global-outlook-for-air-transport---december-2023---report/

Returning from Space: Re-entry. (n.d.). In Space Mission Architecture (p. 4.1.7-309-4.1.7-311). https://www.faa.gov/sites/faa.gov/files/about/office_org/headquarters_offices/avs/III.4.1.7_Returning_from_Space.pdf

Steinbuch, Y. (2018, June 26). Boeing’s concept jet could fly New York to London in 2 hours. New York Post. https://nypost.com/2018/06/26/boeings-concept-jet-could-fly-new-york-to-london-in-2-hours/

Sziroczak, D., Smith, H., & Cranfield University. (2016). A review of design issues specific to hypersonic flight vehicles. In Progress in Aerospace Sciences [Journal-article]. https://dpl6hyzg28thp.cloudfront.net/media/1-s2.0-S0376042115300087-main.pdf

Tobe, R., & Grandhi, R. V. (2013). Hypersonic vehicle thermal protection system model optimization and validation with vibration tests. Aerospace Science and Technology, 28(1), 208–213. https://doi.org/10.1016/j.ast.2012.11.001

Tung Le, V. T., Ha, N. S., & Goo, N. S. (2021). Advanced sandwich structures for thermal protection systems in hypersonic vehicles: A review. Composites. Part B, Engineering, 226, 109301. https://doi.org/10.1016/j.compositesb.2021.109301

Uyanna, O., & Najafi, H. (2020). Thermal protection systems for space vehicles: A review on technology development, current challenges and future prospects. Acta Astronautica, 176, 341–356. https://doi.org/10.1016/j.actaastro.2020.06.047

Yang, X., Gui, Y., Tang, W., Du, Y., Liu, L., Xiao, G., & Dong, W. (2018). Surface thermochemical effects on TPS-coupled aerothermodynamics in hypersonic Martian gas flow. Acta Astronautica, 147, 445–453. https://doi.org/10.1016/j.actaastro.2018.03.055

Zhang, S., Li, X., Qin, J., Qin, J., Cheng, K., Feng, Y., & Bao, W. (2020). Research progress on active thermal protection for hypersonic vehicles. ELSEVIER. https://doi.org/10.1016/j.paerosci.2020.100646

Zhu, L., Li, Y., Gong, L., Chen, X., & Xu, J. (2019). Coupled investigation on drag reduction and thermal protection mechanism induced by a novel combinational spike and multi-jet strategy in hypersonic flows. International Journal of Heat and Mass Transfer/International Journal of Heat and Mass Transfer, 131, 944–964. https://doi.org/10.1016/j.ijheatmasstransfer.2018.11.119

Downloads

Posted

2024-09-25

Categories