ATLAS V Changing it into an RLV for Better Performance

This journal delves into the intricacies of the Atlas V launch vehicle, focusing on four key aspects: propulsion, structure, avionics, and materials. It offers a comprehensive exploration of the Atlas V’s propulsion systems, including the RD-180 and RL-10 engines, as well as the new solid rocket booster. The journal examines the structural components that make up this launch vehicle, highlighting their design and functionality. It delves into the avionics systems that play a critical role in guiding and controlling the Atlas V. Additionally, the journal explores the materials utilized in its construction and their impact on the vehicle’s performance. Together, these components contribute to Atlas V’s aerodynamics Abstract for Atlas V incorporating changes in materials and structure: The utilization of corrugated steel sheets in the construction of the Atlas V rocket’s structure serves a pivotal role in weight reduction, promoting its potential for reusable launches. While retaining durability and safeguarding against insect attacks and algae growth, this innovative application leverages the lightweight nature of the corrugated structure to enhance the rocket’s efficiency. Furthermore, the integration of titanium-nickel alloys in place of traditional materials like aluminum and carbon fiber titanium demonstrates a strategic shift towards enhancing strength, corrosion resistance, and weight balance within the rocket’s components. This substitution capitalizes on the unique properties of these alloys, aligning with the aerospace industry’s ongoing pursuit of improved materials for spacecraft construction. This underscores the profound impact of these material alterations on the Atlas V’s performance, particularly in elevating structural integrity, reducing weight, and advancing reusability—a paradigm shift that augments the rocket’s capabilities in space exploration endeavors.