An engineering evaluation of advanced nuclear thermionic space powerplants
Engineering evaluation of advanced nuclear thermionic space powerplants
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Engineering evaluation of advanced nuclear thermionic space powerplants
Lunar and interplanetary mission-oriented advanced nuclear system parameters - Research and technology implications report
Mission, trajectory, and vehicle details resulting from advanced nuclear propulsion study for Mars and Venus missions
Parametric mission performance data for mission orientated advanced nuclear system parameters study generated by computer simulation of flyby, stopover, and swingby space missions
Summarized study tasks, analyses, and results of advanced nuclear propulsion parameters for Mars and Venus missions
Hydrogen turbopump cycles for obtaining high engine inlet pressures in advanced nuclear rockets, and data on gaseous nuclear reactors and heavy gas containment
Mission, trajectory, and vehicle analyses of manned Mars stopover missions - advanced nuclear system parameters
Advanced control rooms (ACR's) will utilize human-system interface (HSI) technologies that may have significant implications for plant safety in that they will affect the operator's overall role and means of interacting with the system. The Nuclear Regulatory Commission (NRC) reviews the human factors engineering (HFE) aspects of HSI's to ensure that they are designed to good HFE principles and support performance and reliability in order to protect public health and safety. However, the only available NRC guidance was developed more than ten years ago, and does not adequately address the human performance issues and technology changes associated with ACR's. Accordingly, a new approach to ACR safety reviews was developed based upon the concept of 'convergent validity'. This approach to ACR safety reviews is described.
Human exploration of the solar system is limited by our technology, not our imagination. We dream of a time when we can freely travel among the planets and truly become a spacefaring people. However, the current state of our technology limits our options for architecting missions to other planets. Instead of sailing the seas of space in the way that we cruise the seas of Earth, our limited propulsion technology requires us to depart Earth on a giant cluster of gas tanks and return in a lifeboat. This inefficient approach to exploration is evident in many of today's leading mission plans for human flights to Mars, asteroids, and other destinations. The cost and complexity of this approach to mission architecting makes it extremely difficult to realize our dreams of exploration beyond Low Earth Orbit (LEO). This does not need to be the case. Researchers at NASA's Marshall Space Flight Center (MSFC) have been investigating the feasibility of a new take on nuclear propulsion with the performance to enable a paradigm shift in human space exploration. During the fall of 2013, engineers at MSFC's Advanced Concepts Office developed a spacecraft concept (pictured below) around this new propulsion technology and redefined the human Mars mission to show its full potential. This spacecraft, which can be launched with a fleet of soon-to-be available SLS launch vehicles, is fueled primarily with hydrogen, and is fully reusable with no staging required. The reusable nature of this design enables a host of alternative mission architectures that more closely resemble an ocean voyage than our current piecemeal approach to exploration.
In 1989, a Presidential directive created the Space Exploration Initiative (SEI) which had a goal of placing mankind on Mars in the early 21st century. The SEI was effectively terminated in 1992 with the election of a new administration. Although the initiative did not exist long enough to allow substantial technology development, it did provide a venue, for the first time in 20 years, to comprehensively evaluate advanced propulsion concepts which could enable fast, manned transits to Mars. As part of the SEI based investigations, scientists from NASA, DoE National Laboratories, universities, and industry met regularly and proceeded to examine a variety of innovative ideas. Most of the effort was directed toward developing a solid-core, nuclear thermal rocket and examining a high-power nuclear electric propulsion system. In addition, however, an Innovative Concepts committee was formed and charged with evaluating concepts that offered a much higher performance but were less technologically mature. The committee considered several concepts and eventually recommended that further work be performed in the areas of gas core fission rockets, inertial confinement fusion systems, antimatter based rockets, and gas core fission electric systems. Following the committee's recommendations, some computational modeling work has been performed at Los Alamos in certain of these areas and critical issues have been identified.
Mission analysis computer programs for evaluating nuclear engine, vehicle system, and mission parameters for nuclear propulsion system applications in 1975-1990
Nuclear rocket engine for interplanetary missions to Mars and Venus - lunar transfer mission
System and equipment descriptions of manned orbital research laboratory, and interplanetary and lunar ferry vehicles
Analyses of swingby and conjunction class missions, mission aborts, and launch azimuth constraints based on manned Mars stopover missions study
Guidelines and assumptions for manned Mars stopover mission planning analyses - nuclear system parameters
Solid core nuclear reactor engine variables, considering specific impulse, engine weight, operating life and engine thrust
Magnetohydrodynamic generator development and applications in radiating power plants, propellant-cooled propulsion systems, and industry
Design, development, and performance of 35 to 150 kilowatt Brayton power conversion module and application to nuclear reactor powered system