Mars Based Research Articles

A duty to enhance? Genetic engineering for the human Mars settlement.

Humans living off-world will face numerous physical, psychological and social challenges and are likely to suffer negative health effects due to their lack of evolutionary adaptation to space environments. While some of the necessary adaptations may develop naturally over many generations, genetic technologies could be used to speed this process along, potentially improving the wellbeing of early space settlers and their offspring. With broad support, such a program could lead to significant genetic modification of off-world communities, for example, to limit radiation damage on body systems or prevent bone and muscle loss in reduced gravity conditions. Given the extreme stressors of living off-world, and the need to have a healthy workforce to support a fledgling human settlement, those in favour of using genetic technologies to enhance settlers might even claim there is a moral imperative to protect their health in the face of the unique threats of space travel, especially for children born in settlements who did not take on these risks voluntarily. For some, this might simply be an extension of procreative beneficence. However, ethical concerns arise regarding the risks of embracing a eugenicist agenda and the potential impacts on the rights of future settlers to refuse such genetic enhancements for themselves or their children.

A common law in space for public health

Beyond the gravitational pull of Earth, space travel poses substantial public health hazards pertaining to the physical and mental well-being of astronauts and passengers, in addition to a possible threat to the populace of Earth upon re-entry. Exposure to cosmic radiation, cranial pressure from microgravity, weakened immunity to contagion, and the potential for depression and psychosis are all risks. Public health crises of this nature are to be expected as the duration of missions extends, as is the case with Mars settlement. In contrast to national space programmes, which have regarded these obstacles as human factors effecting the mission, public health law in common law British nations approaches them from the perspective of social justice and the preservation of human life and societal welfare. Countries including Australia, Canada, the United States, and the United Kingdom continue to apply traditional common law principles of public health law, which provide a sensible and enduring method for reconciling competing public and private interests. Common law permits the violation of civil liberties through the use of force in public health restraint, forced medication, and quarantine, but only if necessary, reasonable, and equitable. While the understanding of the health challenges associated with long-duration spaceflight may be in its infancy for national space programmes and civilian space ventures, the application of common law public health principles could aid in the establishment of health and safety protocols in which human reactions to crises in space resemble those observed on Earth. This may, nevertheless, necessitate the enactment of a more comprehensive federal public health statute. Embedded in both public health common law and international space law, the pre-eminence of preserving and respecting human life and well-being continues to be a cornerstone of humane justice despite the perilous conditions of space.

Human Evolution, Microgravity, and Challenges Colonizing Mars.

INTRODUCTION: Human colonization of Mars has captured the imagination of many. However, the challenges posed are immense. In microgravity, changes in human physiology, immune dysregulation, alterations of our microbiome, and enhanced virulence of various microbes are some of the barriers that stand in the way of a successful endeavor. Countermeasures can be brought to bear, but it remains unclear if success of such a mission in the foreseeable future is realistic or fanciful.Mermel L. Human evolution, microgravity, and challenges colonizing Mars. Aerosp Med Hum Perform. 2024; 95(9):720-721.

Effects of MgO on the fibre spinnability, mechanical properties and acid resistance of simulated Martian soil

The ultimate goal of Mars exploration is to construct a Mars base. In particular, it is necessary to prepare fibres by using Martian soil as a raw material. High-strength "Martian glass fibres" can be used to reinforce composite materials to meet the requirements of high-strength functional materials in base construction. Owing to the wide variation in MgO content in Martian soil, in this study, the effects of MgO on the structure, strength and acid resistance of "Martian glass and glass fibres" were investigated. The preparation conditions and mechanical properties of simulated Martian soil fibre (SMSF) were studied via DSC, XRD, Raman, NMR, FT-IR and high-temperature rotational viscometry. The corrosion behaviour of MgO-SMSF in H2SO4 solution was subsequently studied via SEM/EDS. The results showed that MgO reduces the spinnability window and prevents the fibres from stretching continuously, and a threshold appears to exist at 10.89 % MgO. The viscosity of the melt decreased significantly, and the crystallization trend increased with MgO above the threshold. The fibre tensile strength showed a nonlinear relationship with a 22.85 % increase in the fibre tensile strength at 9.24 % MgO. SEM/EDS revealed that the surface of the SMSF formed a gel layer, and the mass retention of the MgO-SMSF in the H2SO4 solution reached 90.17 %. The corrosion of SMSF under acidic conditions was controlled by ion diffusion, with Mg+ and Ca+ diffusing to the fibre surface, resulting in nonuniform corrosion. Raman-based statistical structureproperty modelling further explains the impact of MgO-induced structural changes on the tensile strength and elastic modulus, with good agreement between the model predictions and measured values.

Influence of ideas of Russian cosmism on formation and development of scientific and technical elite of rocket engineering and cosmonautics

The article is devoted to the influence of philosophical and theoretical ideas of the scientific direction of Russian cosmism on their transformation into a scientific and practical plane – the creation of the rocket and space industry, the launch of satellites, rockets, and humans into space. The relevance of the problem considered in the article lies in the fact that space, while remaining the sphere of interests of the leading world powers competing with each other in political, economic, cultural, and military terms, remains a platform for international cooperation, on which factors of national and global security largely depend. In this work, space exploration is considered in the development from philosophical and scientific research of the late 19th – early 20th century to projects of private corporations investing in the exploration of the Moon, colonization of Mars, development of a fleet of interstellar ships for travel to the Alpha Centauri system in our days. Scientific novelty is determined by a comprehensive consideration of the dialectics of the intellectual, creative and pragmatic in matters of space exploration. In a short period of time, under the influence of the philosophical ideas of the scientific direction of cosmism, and their logical continuation in the form of the development of the theory of cosmonautics and rocket science, there was the emergence of a new stratum of society – scientific and technical elite, which brought the country to a new level of technical development, which allows it to remain the world's leading space power to this day.

Analysis of Transportation Systems for Colonies on Mars

The colonization of Mars poses unprecedented challenges in developing sustainable and efficient transportation systems to support inter-settlement connectivity and resource distribution. This study conducts a comprehensive evaluation of two proposed transportation systems for Martian colonies: a ground-based magnetically levitated (maglev) train and a low-orbital spaceplane. Through simulation models, we assess the energy consumption, operational and construction costs, and environmental impacts of each system. Monte Carlo simulations further provide insights into the cost variability and financial risk associated with each option over a decade. Our findings reveal that while the spaceplane system offers lower average costs and reduced financial risk, the maglev train boasts greater scalability and potential for integration with Martian infrastructural development. The maglev system, despite its higher initial cost, emerges as a strategic asset for long-term colony expansion and sustainability, highlighting the need for balanced investment in transportation technologies that align with the goals of Martian colonization. Further extending our exploration, this study introduces advanced analysis of alternative transportation technologies, including hyperloop systems, drones, and rovers, incorporating dynamic environmental modeling of Mars and reinforcement learning for autonomous navigation. In an effort to enhance the realism and complexity of our navigation simulation of Mars, we introduce several significant improvements. These enhancements focus on the inclusion of dynamic atmospheric conditions, the simulation of terrain-specific obstacles such as craters and rocks, and the introduction of a swarm intelligence approach for navigating multiple drones simultaneously. This analysis serves as a foundational framework for future research and strategic planning in Martian transportation infrastructure.

Cryogenic Liquid Rocket and Nuclear Thermal Rocket: A Survey of the Current Technology and a Comparison for Future Mars Missions

The innovation of reusable rockets holds the potential to revolutionize both Mars scientific exploration and commercial tourism. Thus, this paper aims to indicate the most promising propulsion system for the Mars mission. While SpaceX proposed the cryogenic liquid rocket Starship to achieve Mars colonization by 2050, the viable nuclear thermal propulsion has been outlined by rocketry experts for space travel. This paper surveys the current state-of-the-art of both popular propulsion systems, indicating their advantages and disadvantages. Methods to increase the delivery and cost efficiency are also offered, including on-orbit refueling for cryogenic liquid rockets and various nuclear core variants for nuclear thermal rockets. Subsequently, their comparative analysis is delivered in the discussion, focusing on their transportation efficiency and cost efficiency for future mass missions. With faster travel, greater payload, and reduced propellant consumption, nuclear thermal propulsion has shown to be a brighter prospect and potential than cryogenic liquid rocket. Nevertheless, the author believes a new class of bimodal nuclear thermal electric propulsion system is the most promising option, combining the merits and complementing drawbacks of cryogenic liquid propulsion, nuclear thermal propulsion, and nuclear electric propulsion.

Review of the technologies and preparations required for Mars colonization

Based on the recent increase in information gained from the growing number of space research missions, many researchers and scholars have begun to reconsider the interplanetary expansion program and have chosen Mars, a resource-rich planet, as a prime research target. The recommendation and implementation of this program need to take into account the needs for long-term space missions, including transportation, equipment, energy, carrying capacity, technology, and life-sustaining carbon, hydrogen, and oxygen. Through the research methods of literature review and theoretical analysis, this paper organizes and analyzes the factors and technological requirements that need to be considered for a long-term space mission, the Transplanetary Colonization Program project, as well as presenting the prerequisites for the colonization of Mars, using the current widely accepted program as a case study. As Mars possesses richer natural resources, the principles needed for transportation survival can be obtained through the exploitation of the resources of Mars itself. Therefore, as a transportation rocket, it can have the greatest flexibility in the design of carrying capacity. In addition, artificial intelligence, 3D printing technology, and nanotechnology are the main priority areas that need to be overcome, which can help in the construction part of the subsequent mission execution.

Research on the feasibility of Mars colonization

Nowadays, the planning on manned mission to Mars from NASA and other institutions have brought interest to Mars again. People wonder if Mars can be the first colony of humanity. To provide an insight to this question, this essay focus on various prospective to discuss whether it is possible for humans to colonize Mars now, or perhaps in the near future. The essay first identifies essential technology needed for a success Mars colonization. Then, examine the past researches to check whether current technology can meet the requirements for Mars colonization. The research finds that the transportation between Earth and Mars is not hard to do, but the efficiency is extremely low by now. Building space stations as intermediates and developing recyclable rocket may help on this problem. When building a settlement on Mars, the life support system will not be a big issue because there are already functional technologies to produce oxygen and plant food on Mars, while water can be extracted from ice sheets on Mars. Meanwhile, requirement for energy can be easily solved by relying on solar energy, wind energy, geothermal energy and nuclear energy. Reconstructing Martian environment is not hard when it comes to altering the atmosphere, but is constructing an artificial magnetosphere is currently unpractical. Mars colonization is still not feasible now, but might be possible within one or two decades.

Moving to Mars: The Feasibility and Desirability of Mars Settlements

The on-going space settlement debate has raised questions whether it is possible to settle other planets, and if it was, is it something humans should do. The problem with this space ethical discussion is that it can easily become too vague. To avoid this problem, we suggest a framework for identifying relevant variables that affect the feasibility constraints and desirability factors of establishing space settlements. The variables we focus on include the settlement stage, scale and time frame. Based on the relevant literature, we take mission cost, survival, habitation, water, in situ resources for food, oxygen and fuel energy and dependence on Earth as feasibility constraints that are relevant for the framework. None of them are hard constraints, but rather soft feasibility constraints that make it difficult to establish a permanent human settlement on Mars in the near- to medium-term future. However, in the past, humanity has achieved goals that first seemed infeasible. To justify the costs and effort, the goal must be highly morally desirable. We discuss five different desirability factors that could help justify the effort but as each framework has unique feasibility constraints, not all of these factors are sufficient or necessary to justify this effort. We argue that some of the desirability factors prominent in space ethical literature are not sufficient or necessary in our framework, and thus, we conclude that the normative grounds for establishing a permanent Mars settlement in the foreseeable future are weak.

Sustainable colonization of Mars using shape optimized structures and in situ concrete

The major obstacle to Martian colonization is the mission cost which requires significant reduction. From the structural engineering point of view, importing materials and structural elements from Earth or massive excavations on the surface of Mars require an enormous amount of energy; thus, inflatable and under-surface structures as the main options for Martian colonization seem unrealistically expensive. Construction of affordable buildings onsite using only in situ sources may represent an ideal solution for Martian colonization. On the other hand, solar energy, at the early stage of colonization, would be the only available, practical, and low-cost energy source on Mars. Though, for sustainable and broad colonization, the energy required for construction and the construction cost should be minimized. Here, we propose three types of simple (relatively optimized), perforated, and algorithmic shape-optimized Martian structures to minimize the material and energy required for construction as well as the construction cost using only in situ resources. These structural forms can be considered remarkable steps towards sustainable structural construction and colonization on Mars. Also, these innovative structures were designed to minimize the tensile stress (maximize the compressive stress) and enable the use of in situ concrete. Our data indicate that compared to our previous study, the material and energy required for construction as well as the construction cost can be reduced by more than 50%. Acceptance criteria and limitations appropriate to the Martian environment, and desirable structural and material behaviors were defined to evaluate whether or not the behavior of a structure under the applied loads and conditions will be acceptable. To detect potential issues for onsite construction and evaluate the geometry of the models, a 1:200 3D model of the best structural form was printed.

Mars mission capabilities enabled by nuclear thermal propulsion

As part of the Artemis era of space exploration, space agencies will be working together with their industry partners to establish systems and infrastructure that enable sustained Lunar missions and develop capabilities for Mars. Lockheed Martin has a longstanding history of designing, building, and operating systems for deep space applications, from Viking to Orion. Lockheed Martin develops concepts, trades, and early system designs for Moon and Mars exploration to enable future missions. In 2016, Lockheed Martin presented a vision for achieving crewed exploration of Mars. Known as Mars Base Camp (MBC), this design reference mission envisioned a crewed vehicle in Martian orbit from which astronauts could perform excursions to Phobos and Deimos and perform telerobotic exploration of the Martian surface, including sample return. This concept served as an “existence proof” for a novel, practical, and affordable path to enable human exploration of the Martian system. In 2017, an update was published that included the production of propellant from water and a single-stage fully reusable Mars lander concept. Then in 2021, Lockheed Martin introduced a nuclear thermal propulsion (NTP) configuration of Mars Base Camp, a technology that will be greatly enabling for crewed missions to Mars. This paper matures the design of the NTP configuration of Mars Base Camp and explores the Mars mission capabilities that the NTP technology will enable. These investigations include optimized trajectories for faster transit to Mars and an analysis of abort scenarios that are made possible by the high thrust and performance of NTP. The results provide insight into the performance and capabilities that are realized when NTP technology is matured and integrated into a Mars transit vehicle. The paper will also describe initial surface infrastructure capabilities that significantly enhance sortie science operations, including mobility and power. The resulting updated Mars Base Camp serves as an example of what is possible with current technologies and technologies under development. The MBC reference mission builds on the capabilities that will be developed and demonstrated through Artemis missions, enabling a viable, sustainable long-term Mars exploration program, with the first crewed Mars mission possible in the 2030s.

Feasibility research on mars colonization by 2060

Exploring the immense cosmos is not just the fundamental survival urge for humans, but also the inescapable final aim of human civilization. Mars exploration will be the first step that human civilization takes to explore this universe because, for one thing, Mars and Earth are the two close planets; for another, Mars is located in the habitable zone in the solar system. This research is aimed to analyze the main problems of human migration to Mars with the current state of technology in a timeframe of a few decades. The research is conducted based on three basic factors for humans to live: water, shelter, and food, with the addition of law to support a colony. The result indicates more research to be conducted due to many unknown factors that will happen in a new environment.

Space hardware for concrete sample production on ISS “MASON concrete mixer”

Advances in space flight technology will enable the construction of Moon or even Mars bases in the not-too-distant future. Thus, materials will be needed that are suitable for building in microgravity environments. One idea is to use concrete, the most used construction material on Earth, for these challenging tasks. The hardening and the properties of concrete under the boundary conditions prevailing on Earth are well understood, but there is only limited research on concrete produced in microgravity. Hence, a research project called MASON was established, which aims to mix and harden concrete on the ISS and to investigate the properties of the specimens made in microgravity extensively. Since a defined geometry of the specimens would be favorable for these investigations, a special hardware was developed, called the MASON Concrete Mixer (MCM), which allows the production of concrete specimens fulfilling the requirements on the geometry as well as the safety requirements. Subsequently, the development, design, tests, and qualification of the MCM as well as its usage are presented.

Risk trade-space analysis for safe human expeditions to Mars

We assessed the integrated safety, health, and performance risk to crews on long-duration missions, specifically to Mars. Using a systems approach rather than one focused on individual countermeasures, we examined the trade space around several such risks to identify high-potential risk mitigation strategies and characterize aspects of Mars mission architectures that could lower aggregated risk. Current Mars Design Reference missions would require durations well over two years and would increase crew exposure to radiation and microgravity well beyond ISS levels, likely resulting in significantly reduced performance beyond our current capability to mitigate that could jeopardize mission success. A “fast Mars transit” round-trip mission concept was studied using an innovative flight dynamics approach to quantify the minimum total mission energy required for a Mars transit with total mission duration less than 400 days. This approach holds promise for sending humans to Mars and returning them safely with acceptable, potentially mitigatable, exposure to microgravity and radiation using current or near-term technologies. The fast transit concept would also result in fewer time-driven vehicle failures and enable sustainable deployment of humans and infrastructure to Mars on a regular cadence, allowing steady exploration and colonization of Mars. Finally, we conclude that reliance on the Low Earth Orbit (LEO) mission operations paradigm – i.e., one of near-complete real-time dependence on experts at Mission Control to manage the combined state of the mission, vehicle, and crew – is high risk given the communication delays and limited resupply of any Mars mission, and this risk is not eliminated by the shorter missions durations of fast transit scenarios. Based on historical trends, it is highly likely that the crew will face a high-consequence problem of uncertain origin during Mars transit when ground support will be greatly reduced. While it may be possible to reduce anomaly rates through improved reliability analysis and testing, and to reduce anomaly impacts through added robustness, such mitigations address only known failure modes and known uncertainties. Therefore, a radical shift in the Human-Systems Integration Architecture (HSIA) that defines the operational paradigm, systems design, and human-systems interactions is required to improve the risk posture to an acceptable level regardless of mission duration.

Radar Observation of the Lava Tubes on the Moon and Mars

The detection of lava tubes beneath the surfaces of the Moon and Mars has been a popular research topic and challenge in planetary radar observation. In recent years, the Moon–based ground penetrating radar (GPR) carried by the Chinese Chang’e–3/–4 mission, the RIMFAX radar carried by the Mars mission Perseverance, and the RoSPR radar and MOSIR radar carried by China’s Tianwen–1 orbiter have extensively promoted the exploration of the underground space of extraterrestrial bodies, which is crucial for the future utilization and development of these spaces. This paper expounds on the principles, methods, and detection results of using GPR to detect lava tubes on the Moon and Mars. First, lava tubes’ formation mechanism and morphological characteristics are outlined, followed by an introduction to GPR’s working principles and classification. The advantages, disadvantages, and prospects of different types of radar in detecting the lava tubes are analyzed. Finally, the distribution of lava tubes on the Moon and Mars is briefly summarized, and the potential utilization of lava tubes is discussed. We believe that the GPR technique is an effective geophysical method for exploring the underground structures of the Moon and Mars, and the lava tubes beneath the surface of extraterrestrial bodies can provide important references for selecting future Moon and Mars bases.

Sustaining a Mars Colony through Integration of Single-cell Protein and Oil Production in Food Supply Chains

As humanity sets its sights on establishing a sustainable and prosperous colony on Mars, one of the key challenges to overcome is ensuring a reliable and nutritious food supply for settlers. While various solutions for food production on Mars have been proposed, there is a growing interest in the use of microorganisms as a means of producing essential nutrients. This review article highlights the advantages of utilizing single-cell protein and single-cell oil technologies to produce essential amino acids and fatty acids for the food supply chains of a Mars colony. We provide an analysis of the potential benefits, challenges and limitations of these solutions and outline the necessary steps to be taken in order to successfully integrate them into the infrastructure of a Martian settlement.

Perfect Preparation.

Perfect Preparation.

Multiphysics simulations of Self-Regulating performance of an optimized molten metal fuel microreactor design

Advanced microreactors are expected to play an indispensable role in reliable energy solutions for civilian/military applications in off-grid regions and space applications such as power supplies for Lunar and Mars bases. An innovative fast neutron spectrum heat pipe microreactor (HP-MR) concept was recently proposed with two unique features: molten U-Mn fuel and heat pipes as the heat removal mechanism. The microreactor was designed to be self-regulated, solely relying on reactivity feedbacks from fuel temperature. The reactor design has been further optimized to provide sufficient engineering safety margin and effective heat removal. In this study, the self-regulating performance of the optimized molten metal fuel microreactor was investigated by multiphysics simulations (neutronics, heat-transfer and heat pipe modeling) based on the MOOSE MultiApps system. The responses of the reactor to a series of transient scenarios were simulated to demonstrate the exceptional and inherent safety features of the novel microreactor concept.

A Mighty Cooperative

A Mighty Cooperative