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Stream/Area:
-
Subject:
-
Paper ID:
IJSREM27498
Volume:
7 |
12 |
Dec 2023
Pages:
Publication Frequency:
Monthly (12 issues per year)
License:International Journal of Scientific Research in Engineering and Management follows the Creative Commons Attribution 4.0 (CC BY 4.0) License, allowing free use and distribution with proper attribution.
The continued evolution of reusable rocket launch vehicles is creating a paradigm shift in space exploration that requires a comprehensive re-evaluation of aerodynamic design principles. This study addresses the complex interplay between aerodynamics and the sustainable development of reusable rocket launch vehicles, and highlights the significant challenges and unprecedented opportunities associated with this transformative journey. One of the biggest challenges is dealing with the complex flow phenomena encountered during launch and reentry. The complex interactions between shock waves, boundary layers and pillars require innovative aerodynamic solutions to optimize vehicle performance and ensure structural integrity. In addition, the harsh thermal environment experienced during atmospheric re-entry poses a major obstacle, necessitating the development of robust thermal protection systems that can withstand extreme temperatures and ensure cargo safety. In addition, the pursuit of cost-effective and sustainable access to space requires the exploration of new aerodynamic technologies. Active flow control mechanisms, including advanced control surfaces and flow manipulation techniques, offer promising tools to improve vehicle maneuverability and efficiency during launch and reentry phases. At the same time, the integration of advanced materials such as lightweight composites and advanced ceramics has the potential to enhance structural flexibility while minimizing overall vehicle mass, thereby optimizing fuel consumption and operating costs. decreases. Additionally, this brief highlights opportunities to use advanced computational fluid dynamics simulations and wind tunnel testing to improve aerodynamic design parameters, simplify development programs, and accelerate the realization of next-generation rocket launch vehicles. By adopting a multidisciplinary approach that combines aerodynamics, materials science, and computational modeling, the aerospace industry opens
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Publication Date
12/16/2023
Peer Review Type
Double-Blind Peer Review
Review Rounds: 2
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Conflict of Interest
The authors declare no conflict of interest related to this research work.
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No funding information available for this research.
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