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  • 1
    Publication Date: 2020-08-01
    Print ISSN: 1270-9638
    Electronic ISSN: 1626-3219
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Published by Elsevier
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  • 2
    Publication Date: 2019-06-01
    Print ISSN: 0094-5765
    Electronic ISSN: 1879-2030
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Published by Elsevier
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  • 3
    Publication Date: 2019-07-13
    Description: A human mission to Mars will occur at some time in the coming decades. When it does, it will be the end result of a complex network of interconnected design choices, systems analyses, technical optimizations, and non-technical compromises. This mission will extend the technologies, engineering design, and systems analyses to new limits, and may very well be the most complex undertaking in human history. It can be illustrated as a large menu, or as a large decision tree. Whatever the visualization tool, there are numerous design decisions required to assemble a human Mars mission, and many of these interconnect with one another. This paper examines these many decisions and further details a number of choices that are highly interwoven throughout the mission design. The large quantity of variables and their interconnectedness results in a highly complex systems challenge, and the paper illustrates how a change in one variable results in ripples (sometimes unintended) throughout many other facets of the design. The paper concludes with a discussion of some mission design variables that can be addressed first, and those that have already been addressed as a result of ongoing National Aeronautics and Space Administration (NASA) developments, or as a result of decisions outside the technical arena. It advocates the need for a 'reference design' that can be used as a point of comparison, and to illustrate the system-wide impacts as design variables change.
    Keywords: Systems Analysis and Operations Research; Lunar and Planetary Science and Exploration
    Type: JSC-CN-40444 , International Astronautical Congress (IAC); Sep 25, 2017 - Sep 29, 2017; Adelaide; Australia
    Format: application/pdf
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  • 4
    Publication Date: 2019-07-13
    Description: As we venture back to the Moon with a longer term goal of future Mars missions, lunar missions can provide an important testbed for technologies, systems and operations that directly feed forward to future Mars needs. Gateway missions can provide good in-space transportation feed forward to human Mars missions. Modest operations on the Moon such as the GER (Global Exploration Roadmap)-class missions, can provide key Mars human performance and surface mission capability development and risk reduction. A human return to the Moon can, if done correctly, serve as an excellent down payment to Mars.
    Keywords: Lunar and Planetary Science and Exploration
    Type: JSC-E-DAA-TN61646-1 , International Astronautical Congress (IAC 2018); Oct 01, 2018 - Oct 05, 2018; Bremen; Germany
    Format: application/pdf
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  • 5
    Publication Date: 2019-07-13
    Description: Human space mission designers stretching back to von Braun and beyond have envisioned the moon as a waypoint to the more challenging missions to Mars. The moon is seen as a potential proving ground for technologies, equipment and operations, and a venue upon which to learn the art of surface exploration. Mars missions are years in duration with very limited Earth return opportunities, but the moon provides the opportunity to perfect exploration concepts while being only a few days from Earth. Though the environment and gravity differ from Mars, and will thereby not provide a perfectly analogous environment, the remoteness, limited logistics, and harsh conditions on the Moon provide an environment that can be used to stress many systems that will be used or will be extensible to hardware and operations that will be used on Mars. This paper begins by describing the systems, or options for systems, that together comprise a human Mars architecture. With this human Mars operational concept as a basis of comparison, each of these systems is analyzed in the context of a range of potential exploration missions that first targets lunar exploration experience, examining how the lunar experience can be best used to prepare for the eventual human mission to Mars. The paper concludes with a concise summary of specific areas that have the strongest applicability between exploration experience on the lunar surface and extensibility to human Mars exploration.
    Keywords: Lunar and Planetary Science and Exploration
    Type: IAC-18/A3,1,3,x43905 , JSC-E-DAA-TN61646-2 , International Astronautical Congress (IAC 2018); Oct 01, 2018 - Oct 05, 2018; Bremen; Germany
    Format: application/pdf
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  • 6
    Publication Date: 2019-08-13
    Description: NASA/JSC is implementing an advanced propulsion physics laboratory, informally known as "Eagleworks", to pursue propulsion technologies necessary to enable human exploration of the solar system over the next 50 years, and enabling interstellar spaceflight by the end of the century. This work directly supports the "Breakthrough Propulsion" objectives detailed in the NASA OCT TA02 In-space Propulsion Roadmap, and aligns with the #10 Top Technical Challenge identified in the report. Since the work being pursued by this laboratory is applied scientific research in the areas of the quantum vacuum, gravitation, nature of space-time, and other fundamental physical phenomenon, high fidelity testing facilities are needed. The lab will first implement a low-thrust torsion pendulum (〈1 uN), and commission the facility with an existing Quantum Vacuum Plasma Thruster. To date, the QVPT line of research has produced data suggesting very high specific impulse coupled with high specific force. If the physics and engineering models can be explored and understood in the lab to allow scaling to power levels pertinent for human spaceflight, 400kW SEP human missions to Mars may become a possibility, and at power levels of 2MW, 1-year transit to Neptune may also be possible. Additionally, the lab is implementing a warp field interferometer that will be able to measure spacetime disturbances down to 150nm. Recent work published by White [1] [2] [3] suggests that it may be possible to engineer spacetime creating conditions similar to what drives the expansion of the cosmos. Although the expected magnitude of the effect would be tiny, it may be a "Chicago pile" moment for this area of physics.
    Keywords: Space Sciences (General)
    Type: JSC-CN-25207 , JANNAF Joint Propulsion Meeting; Dec 05, 2011 - Dec 09, 2011; Huntsville, AL; United States
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  • 7
    Publication Date: 2019-07-12
    Description: The exploration of Mars by human crews will be a complex endeavor as illustrated by this description of NASA's current architecture for the human exploration of the surface of Mars. The surface environment, in particular the ubiquitous dust, will be an important factor in designing the systems and operations needed for a safe and effective campaign of missions to achieve this objective. This introduction describes the exploration architecture with some indication of where and how dust could affect it. The remainder of this volume describes details of these dust effects on the crews, the systems, and the operations that make up this exciting and challenging enterprise.
    Keywords: Lunar and Planetary Science and Exploration
    Type: JSC-E-DAA-TN53297
    Format: application/pdf
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