Power System Design for a Jupiter Solar Electric Propulsion Spacecraft

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (777 download)

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Book Synopsis Power System Design for a Jupiter Solar Electric Propulsion Spacecraft by : V. Truscello

Download or read book Power System Design for a Jupiter Solar Electric Propulsion Spacecraft written by V. Truscello and published by . This book was released on 1968 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Spacecraft Power Systems

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Publisher : CRC Press
ISBN 13 : 1003804217
Total Pages : 363 pages
Book Rating : 4.0/5 (38 download)

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Book Synopsis Spacecraft Power Systems by : Mukund R. Patel

Download or read book Spacecraft Power Systems written by Mukund R. Patel and published by CRC Press. This book was released on 2023-12-12 with total page 363 pages. Available in PDF, EPUB and Kindle. Book excerpt: This second edition of Spacecraft Power Systems is a comprehensive coverage of the fundamentals, design trades, components, controls, and operations of spacecraft power systems based on the real-world design and operations of spacecraft that have successfully flown for decades. It also includes emerging high-voltage, high-power systems for in-space propulsion for interplanetary travel. With new and updated chapters, sections, and discussions, the second edition covers up-to-date high-voltage, MW-scale electric propulsion, updated PV and battery systems, spacecraft power components, power electronics, and their architectures and operations. This book also presents the latest in spacecraft design processes and trades, controls, operations, and protection. This book is intended for senior undergraduate and graduate students in mechanical, aerospace, and electrical engineering taking courses in Space Systems, Space Engineering, and Spacecraft Power Systems, as well as for practicing aerospace and power engineers and managers who are designing, developing, and operating spacecraft power systems.

Effect of Voltage Level on Power System Design for Solar Electric Propulsion Missions

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781721572557
Total Pages : 34 pages
Book Rating : 4.5/5 (725 download)

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Book Synopsis Effect of Voltage Level on Power System Design for Solar Electric Propulsion Missions by : National Aeronautics and Space Administration (NASA)

Download or read book Effect of Voltage Level on Power System Design for Solar Electric Propulsion Missions written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-20 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents study results quantifying the benefits of higher voltage, electric power system designs for a typical solar electric propulsion spacecraft Earth orbiting mission. A conceptual power system architecture was defined and design points were generated for system voltages of 28-V, 50-V, 120-V, and 300-V using state-of-the-art or advanced technologies. A 300-V 'direct-drive' architecture was also analyzed to assess the benefits of directly powering the electric thruster from the photovoltaic array without up-conversion. Fortran and spreadsheet computational models were exercised to predict the performance and size power system components to meet spacecraft mission requirements. Pertinent space environments, such as electron and proton radiation, were calculated along the spiral trajectory. In addition, a simplified electron current collection model was developed to estimate photovoltaic array losses for the orbital plasma environment and that created by the thruster plume. The secondary benefits of power system mass savings for spacecraft propulsion and attitude control systems were also quantified. Results indicate that considerable spacecraft wet mass savings were achieved by the 300-V and 300-V direct-drive architectures. Kerslake, Thomas W. Glenn Research Center NASA/TM-2003-212304, E-13876, NAS 1.15:212304

Effect of Voltage Level on Power System Design for Solar Electric Propulsion Missions

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effect of Voltage Level on Power System Design for Solar Electric Propulsion Missions by :

Download or read book Effect of Voltage Level on Power System Design for Solar Electric Propulsion Missions written by and published by . This book was released on 2003 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Solar Power System Options for the Radiation and Technology Demonstration Spacecraft

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Publisher :
ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Solar Power System Options for the Radiation and Technology Demonstration Spacecraft by :

Download or read book Solar Power System Options for the Radiation and Technology Demonstration Spacecraft written by and published by . This book was released on 2000 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Interplanetary Probe Missions with Solar-electric Propulsion Systems

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Interplanetary Probe Missions with Solar-electric Propulsion Systems by : Charles L. Zola

Download or read book Interplanetary Probe Missions with Solar-electric Propulsion Systems written by Charles L. Zola and published by . This book was released on 1969 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Early Application of Solar-electric Propulsion to a 1-astronomical-unit Out-of-the-ecliptic Mission

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Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Early Application of Solar-electric Propulsion to a 1-astronomical-unit Out-of-the-ecliptic Mission by : William C. Strack

Download or read book Early Application of Solar-electric Propulsion to a 1-astronomical-unit Out-of-the-ecliptic Mission written by William C. Strack and published by . This book was released on 1970 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Current technology for solar-electric propulsion is used to assess the potential performance advantages of low-thrust propulsion for an out-of-the-ecliptic mission. Simple normal-to-the-orbit thrust steering is assumed with coast subarcs permitted. The electric spacecraft is launched onto an Earth escape trajectory by an Atlas (SLV3C)-Centaur or a Titan IIIC. Comparisons with a similarly launched uprated Burner II stage reveal that significant performance gains are possible using the electric stage with 250- to 475-day flight times.

Effect Of Voltage Level On Power System Design For Solar Electric Propulsion Missions... NASA/TM-2003-212304... National Aeronautics And Space Administration... April 2003

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (589 download)

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Book Synopsis Effect Of Voltage Level On Power System Design For Solar Electric Propulsion Missions... NASA/TM-2003-212304... National Aeronautics And Space Administration... April 2003 by : United States. National Aeronautics and Space Administration

Download or read book Effect Of Voltage Level On Power System Design For Solar Electric Propulsion Missions... NASA/TM-2003-212304... National Aeronautics And Space Administration... April 2003 written by United States. National Aeronautics and Space Administration and published by . This book was released on 2003* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Mass Study for Modular Approaches to a Solar Electric Propulsion Module

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781725989924
Total Pages : 38 pages
Book Rating : 4.9/5 (899 download)

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Book Synopsis Mass Study for Modular Approaches to a Solar Electric Propulsion Module by : National Aeronautics and Space Administration (NASA)

Download or read book Mass Study for Modular Approaches to a Solar Electric Propulsion Module written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-22 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The propulsion module comprises six to eight 30-cm thruster and power processing units, a mercury propellant storage and distribution system, a solar array ranging in power from 18 to 25 kW, and the thermal and structure systems required to support the thrust and power subsystems. Launch and on-orbit configurations are presented for both modular approaches. The propulsion module satisfies the thermal design requirements of a multimission set including: Mercury, Saturn, and Jupiter orbiters, a 1-AU solar observatory, and comet and asteroid rendezvous. A detailed mass breakdown and a mass equation relating the total mass to the number of thrusters and solar array power requirement is given for both approaches. Sharp, G. R. and Cake, J. E. and Oglebay, J. C. and Shaker, F. J. Glenn Research Center NASA-TM-X-3473, E-8800 RTOP 506-22...

Solar Power System Analyses for Electric Propulsion Missions

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ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Solar Power System Analyses for Electric Propulsion Missions by :

Download or read book Solar Power System Analyses for Electric Propulsion Missions written by and published by . This book was released on 1999 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Solar Electric Propulsion Mission Architectures

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781721583942
Total Pages : 34 pages
Book Rating : 4.5/5 (839 download)

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Book Synopsis Solar Electric Propulsion Mission Architectures by : National Aeronautics and Space Administration (NASA)

Download or read book Solar Electric Propulsion Mission Architectures written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-20 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: This presentation reviews Solar Electric Propulsion (SEP) Mission Architectures with a slant towards power system technologies and challenges. The low-mass, high-performance attributes of SEP systems have attracted spacecraft designers and mission planners alike and have led to a myriad of proposed Earth orbiting and planetary exploration missions. These SEP missions are discussed from the earliest missions in the 1960's, to first demonstrate electric thrusters, to the multi-megawatt missions envisioned many decades hence. The technical challenges and benefits of applying high-voltage arrays, thin film and low-intensity, low-temperature (LILT) photovoltaics, gossamer structure solar arrays, thruster articulating systems and microsat systems to SEP spacecraft power system designs are addressed. The overarching conclusion from this review is that SEP systems enhance, and many times enable, a wide class of space missions. Kerslake, Thomas W. Glenn Research Center NASA/TM-2003-212456, NAS 1.15:212456, E-13995

Electrical Power Generation Systems for Space Applications

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Electrical Power Generation Systems for Space Applications by : United States. National Aeronautics and Space Administration

Download or read book Electrical Power Generation Systems for Space Applications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1965 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Structural Design Concepts for a Multi-megawatt Solar Electric Propulsion (SEP) Spacecraft

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Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Structural Design Concepts for a Multi-megawatt Solar Electric Propulsion (SEP) Spacecraft by :

Download or read book Structural Design Concepts for a Multi-megawatt Solar Electric Propulsion (SEP) Spacecraft written by and published by . This book was released on 1991 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Solar Energy Update

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ISBN 13 :
Total Pages : 380 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Solar Energy Update by :

Download or read book Solar Energy Update written by and published by . This book was released on 1978 with total page 380 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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Publisher :
ISBN 13 :
Total Pages : 856 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1969 with total page 856 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Proceedings of the ... Intersociety Energy Conversion Engineering Conference

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Publisher :
ISBN 13 :
Total Pages : 518 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Proceedings of the ... Intersociety Energy Conversion Engineering Conference by :

Download or read book Proceedings of the ... Intersociety Energy Conversion Engineering Conference written by and published by . This book was released on 1982 with total page 518 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Advanced Electric Propulsion for Space Solar Power Satellites

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Publisher : Independently Published
ISBN 13 : 9781724011138
Total Pages : 32 pages
Book Rating : 4.0/5 (111 download)

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Book Synopsis Advanced Electric Propulsion for Space Solar Power Satellites by : National Aeronautics and Space Adm Nasa

Download or read book Advanced Electric Propulsion for Space Solar Power Satellites written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-25 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The sun tower concept of collecting solar energy in space and beaming it down for commercial use will require very affordable in-space as well as earth-to-orbit transportation. Advanced electric propulsion using a 200 kW power and propulsion system added to the sun tower nodes can provide a factor of two reduction in the required number of launch vehicles when compared to in-space cryogenic chemical systems. In addition, the total time required to launch and deliver the complete sun tower system is of the same order of magnitude using high power electric propulsion or cryogenic chemical propulsion: around one year. Advanced electric propulsion can also be used to minimize the stationkeeping propulsion system mass for this unique space platform. 50 to 100 kW class Hall, ion, magnetoplasmadynamic, and pulsed inductive thrusters are compared. High power Hall thruster technology provides the best mix of launches saved and shortest ground to Geosynchronous Earth Orbital Environment (GEO) delivery time of all the systems, including chemical. More detailed studies comparing launch vehicle costs, transfer operations costs, and propulsion system costs and complexities must be made to down-select a technology. The concept of adding electric propulsion to the sun tower nodes was compared to a concept using re-useable electric propulsion tugs for Low Earth Orbital Environment (LEO) to GEO transfer. While the tug concept would reduce the total number of required propulsion systems, more launchers and notably longer LEO to GEO and complete sun tower ground to GEO times would be required. The tugs would also need more complex, longer life propulsion systems and the ability to dock with sun tower nodes. Oleson, Steve Glenn Research Center NASA/TM-1999-209307, E-11833, NAS 1.15:209307, AIAA Paper 99-2872