Hypersonic High Speed Strike Weapons: Design, Research and Development

Authors

DOI:

https://doi.org/10.61359/11.2106-2461

Keywords:

Hypersonic, Weapons, HHSSW, Space Warfare, Asteroid, Space Mining

Abstract

Hypersonic High-Speed Strike Weapons are a part of advanced weapon technology used in military engagements, designed to travel and sustain speeds of at least Mach 5, which is five times the speed of sound. These specially designed weapons are capable of maneuvering and changing directions unpredictably. In this paper, we explore the advantages of using such weapons, the research behind them, and how their implementation could enhance military engagements. By employing this system of weapons, we can expect quick weapon system activation times and precise deployment regarding targets. This study examines the design, overview, technical aspects, feasibility, advantages, and disadvantages of deploying this weapon technology in real-time use. However, several challenges must be addressed to successfully deploy these weapons systems. The primary challenges associated with the deployment of hypersonic weapons include temperature management, propulsion technology, material science (which is critical due to the high-speed demands), safety and reliability, strategic and ethical considerations, financial and time constraints, testing facilities, and the guidance and control of these systems. Overcoming these challenges through advanced technology and innovative ideas is essential for the successful implementation of Hypersonic High-Speed Strike Weapons (HHSSW) systems. The HHSSW systems hold promise for advancing the current weapons technology that humanity possesses. With proper research and resource allocation for HHSSW systems, we can anticipate their development for applications such as asteroid or comet deflection and, if necessary, space warfare.

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Published

2024-10-30

How to Cite

Kalvinkar, M., Jacob, K., Prajwal Reddy, & Kruthik R. (2024). Hypersonic High Speed Strike Weapons: Design, Research and Development. Acceleron Aerospace Journal, 3(5), 593–599. https://doi.org/10.61359/11.2106-2461