Theoretical Design and Overview of Steam Propelled and Nuclear Powered Interplanetary Transit Vehicle for Human Crewed Extraterrestrial Exploration

Authors

DOI:

https://doi.org/10.61359/11.2106-2405

Keywords:

Interplanetary Missions, Spaceship, Steam Propulsion, Interplanetary Transit Vehicle, Interplanetary Spacecraft

Abstract

This article provides a theoretical overview of a spacecraft that utilizes extraterrestrial water resources and controlled nuclear fission to propel itself during interplanetary travel. The spacecraft is equipped with a water extraction module to supply water to a large water-boiler container, a small nuclear reactor, a nuclear heat coupler, and an exhaust nozzle for steam propulsion. When the reactor is activated, the water is transformed into steam through nuclear heat and is stored in a pressurized steam chamber. Once the steam reaches a specific pressure limit, it is released through the nozzle, resulting in steam propulsion and the movement of the spacecraft. The velocity of the spacecraft can be adjusted by controlling the injection of steam into the propulsion chamber. In this study, we have examined the feasibility, design overview, and constraints associated with constructing this type of spacecraft in Low Earth Orbit (LEO). The proposed spacecraft aims to provide faster and more reliable interplanetary transit beyond Mars, utilizing renewable energy resources. Since water resources can be found beyond Mars through asteroids, comets, and moons, the challenge lies not in finding water but in the extraction process. Furthermore, the scientific community requires faster transit vehicles for human exploration of Mars and Ceres. However, no architecture has been proposed for crewed exploration beyond this point. Ultimately, it is hoped that this type of spacecraft will enable future astronauts to undertake deep space exploration missions in the coming decades. The manuscript will delve into the design strategy, challenges, launch vehicles needed for deploying assembling instruments, and the assessment of dimensions and crew capability.

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Author Biographies

Malaya Kumar Biswal M, Founder and CEO, Acceleron Aerospace, Bangalore, Karnataka, India - 560037

Malaya Kumar Biswal is the Founder & CEO of Acceleron Aerospace in Bangalore, India. He is a renowned entrepreneur and scientist in aerospace engineering, specializing in space exploration. After earning his bachelor's degree in Aerospace Engineering, he worked as a Senior Research Scientist at Grahaa Space, focusing on satellite reliability, aerospace design, and space science research. With a visionary mindset, Biswal founded Acceleron Aerospace and now leads the company in revolutionizing the aerospace industry. He is particularly interested in human Mars exploration and envisions ambitious missions to Mars and Ceres. Biswal's achievements have earned him respect in the scientific community, and he actively mentors aspiring scientists, inspiring future space pioneers.

Ilavazhagi G, Director, Acceleron Aerospace, Bangalore, Karnataka, India - 560037

Ilavazhagi G, with a Masters in English and a Bachelor's in Education, serves as the Director of Acceleron Aerospace in Bangalore, India. Notably contributing to "A Comprehensive Overview of ISRO's Ambitious Space Station Project," she blends literary insight with aerospace leadership. Ilavazhagi G is dedicated to advancing space education and empowering women in STEM. Her role as a women entrepreneur underscores her commitment to breaking barriers in the aerospace industry, making her a dynamic force at the intersection of literature, education, and space exploration.

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Published

2024-01-30

How to Cite

Biswal M, M. K., & Ilavazhagi G. (2024). Theoretical Design and Overview of Steam Propelled and Nuclear Powered Interplanetary Transit Vehicle for Human Crewed Extraterrestrial Exploration. Acceleron Aerospace Journal, 2(1), 150–155. https://doi.org/10.61359/11.2106-2405