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  • 1
    Publication Date: 2019-07-13
    Description: Use of high-power solar arrays, at power levels ranging from approximately 500 KW to several megawatts, has been proposed for a solar-electric propulsion (SEP) demonstration mission, using a photovoltaic array to provide energy to a high-power xenon-fueled engine. One of the proposed applications of the high-power SEP technology is a mission to rendezvous with an asteroid and move it into lunar orbit for human exploration, the Asteroid Retrieval mission. The Solar Electric Propulsion project is dedicated to developing critical technologies to enable trips to further away destinations such as Mars or asteroids. NASA needs to reduce the cost of these ambitious exploration missions. High power and high efficiency SEP systems will require much less propellant to meet those requirements.
    Keywords: Spacecraft Propulsion and Power
    Type: GRC-E-DAA-TN23902 , IEEE Photovoltaic Specialists Conference (PVSC); Jun 14, 2015 - Jun 19, 2015; New Orleans, LA; United States
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-13
    Description: NASA Glenn Research Center (GRC) has a long history related to the development of advanced power technology for space applications. This expertise covers the breadth of energy generation (photovoltaics, thermal energy conversion, etc.), energy storage (batteries, fuel cell technology, etc.), power management and distribution, and power systems architecture and analysis. Such advanced technology is now being developed for small satellite and cubesat applications and could have a significant impact on the longevity and capabilities of these missions. A presentation during the Pre-Conference Workshop will focus on various advanced power technologies being developed and demonstrated by NASA, and their possible application within the small satellite community.
    Keywords: Spacecraft Propulsion and Power
    Type: GRC-E-DAA-TN45147 , Annual AIAA/USU Conference on Small Satellites; Aug 05, 2017 - Aug 10, 2017; Logan, UT; United States
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  • 3
    Publication Date: 2019-07-13
    Description: The Triton Hopper is a concept for a vehicle to explore the surface of Neptunes moon Triton, which uses a radioisotope heated rocket engine and in-situ propellant acquisition. The initial Triton Hopper conceptual design stores pressurized Nitrogen in a spherical tank to be used as the propellant. The aim of the research was to investigate the benefits of storing propellant at ambient temperature and heating it through a thermal block during engine operation, as opposed to storing gas at a high temperature.
    Keywords: Spacecraft Propulsion and Power
    Type: GRC-E-DAA-TN38020 , AIAA Science and Technology Forum and Expo 2017; Jan 09, 2017 - Jan 13, 2017; Grapevine, TX; United States
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  • 4
    Publication Date: 2019-11-14
    Description: The Triton Hopper is a NASA Innovative Advanced Concepts (NIAC) project to design a mission to not merely land, but repeatedly fly across the surface of Triton, utilizing the volatile surface ices (primarily nitrogen) as propellant for a radioisotope-heated thermal rocket engine to launch across the surface and explore all the moon's varied terrain. An engineering design study of the vehicle and mission was done. With a calculated range of 20 km per hop, equator-to-pole mobility can be achieved over a primary mission duration of 2 years. Using Nuclear Electric Propulsion for the transfer vehicle, the same concept can be applied for a mission to the surface of Pluto.
    Keywords: Spacecraft Propulsion and Power
    Type: IAC-19,A3,5,7,x53412 , GRC-E-DAA-TN74147 , International Astronautical Congress (IAC) Conference; Oct 21, 2019 - Oct 25, 2019; Washington, DC; United States
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  • 5
    Publication Date: 2019-12-13
    Description: As first analyzed by Hermann Bondi in 1957, matter with negative mass is consistent with the structure of Einstein's general theory of Relativity. Although initially the concept was considered just a theoretical curiosity, negative mass, or "exotic matter," is now incorporated into the body of mainstream physics in a number of forms. Negative mass has a number of rather non-intuitive properties, which, as first noted by Bondi, and then later commented on by Forward (1990), Landis (1991), and others, results in possible applications for propulsion requiring little, or possibly no, expenditure of fuel. As pointed out by Morris and Thorne (1988) and others, negative mass (or, more strictly, a violation of the null energy condition) is also a requirement for any proposed faster than light travel. This paper presents the basic theory of negative mass, the ways by which it can manifest in contemporary physical theory, and the counterintuitive properties that result, including possible uses for interstellar propulsion. Although negative mass has moved from a theoretical curiosity to a concept fundamental to the contemporary understanding of physics, it is still not clear whether bulk negative mass can be manufactured, or if it is limited to only appearing at the cosmological scale (e.g., dark energy:) or in the quantum (e.g., Casimir vacuum) limit. If it can be manufactured, the propulsion applications would be significant.
    Keywords: Spacecraft Propulsion and Power
    Type: GRC-E-DAA-TN75591 , Interstellar Symposium and Advanced Interstellar Propulsion Workshop; Nov 10, 2019 - Nov 15, 2019; Wichita, KS; United States
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  • 6
    Publication Date: 2019-12-13
    Description: In the last few years, the concept that an ultra-lightweight probe could be sent to one of the nearby stars pushed by a laser beam reflecting from a lightweight sail has moved from science fiction into conceptual design. A candidate interstellar sail envisions a two- to three-gram "starchip" micro probe, flying past a planet of Proxima Centauri after a 20 year voyage. With the probe moving at 60,000 km/sec, the flyby encounter at the target planet is within 1 AU of the target planet at most a few hours, and in the case of an encounter with a planet of Proxima Centauri, is close to the star for only a few minutes. With current technology, no power system exists that can produce the required power with a mass of less than one gram.
    Keywords: Spacecraft Propulsion and Power
    Type: GRC-E-DAA-TN75407 , Interstellar Symposium; Nov 10, 2019 - Nov 15, 2019; Whichita, KS; United States
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