Revolutionary Propulsion Research at Tu Dresden
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Experimental Confirmation of Weber Electrodynamics Against Maxwell Electrodynamics
Experimental confirmation of Weber electrodynamics against Maxwell electrodynamics Steffen Kuhn¨ steff[email protected] April 25, 2019 This article examines by means of an easily reproducible experiment whether Maxwell electrodynamics or the almost forgotten Weber electro- dynamics of Carl Friedrich Gauss and Wilhelm Weber is correct. For this purpose, it is shown that when charging a capacitor with two very flat and horizontally aligned plates a force on a permanent magnet should arise be- tween the plates which differs in both theories diametrically in its direction. Subsequently, the measurement setup is described and, based on the mea- surement results, it is determined that Maxwell electrodynamics contradicts the experiment. The result of the experiment suggests that all aspects of modern physics should be subjected to a careful and critical review. Contents 1 Introduction2 2 Basics 3 2.1 The force between two uniformly moving point charges...........3 2.1.1 Weber force...............................3 2.1.2 Maxwell force..............................3 2.2 Forces between current elements.......................5 2.3 Magnetic forces in a wire gap.........................5 2.4 Solution of Maxwell's equations for a wire stub............... 10 3 Experiment 13 3.1 Experimental setup............................... 13 3.2 Measurement results and evaluation..................... 15 1 4 Summary and conclusion 17 1 Introduction Maxwell's equations have been very successful in describing electromagnetic waves for more than one hundred years. Their rise to the sole theory of electromagnetism be- gins with an article by James Clerk Maxwell in 1865 [Maxwell, 1865]. In this article he shows that from the complete set of Maxwell's equations, including the displacement current, a wave equation can be derived in which electromagnetic disturbances of the field propagate at the speed of light. -
Magnetoshell Aerocapture: Advances Toward Concept Feasibility
Magnetoshell Aerocapture: Advances Toward Concept Feasibility Charles L. Kelly A thesis submitted in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics & Astronautics University of Washington 2018 Committee: Uri Shumlak, Chair Justin Little Program Authorized to Offer Degree: Aeronautics & Astronautics c Copyright 2018 Charles L. Kelly University of Washington Abstract Magnetoshell Aerocapture: Advances Toward Concept Feasibility Charles L. Kelly Chair of the Supervisory Committee: Professor Uri Shumlak Aeronautics & Astronautics Magnetoshell Aerocapture (MAC) is a novel technology that proposes to use drag on a dipole plasma in planetary atmospheres as an orbit insertion technique. It aims to augment the benefits of traditional aerocapture by trapping particles over a much larger area than physical structures can reach. This enables aerocapture at higher altitudes, greatly reducing the heat load and dynamic pressure on spacecraft surfaces. The technology is in its early stages of development, and has yet to demonstrate feasibility in an orbit-representative envi- ronment. The lack of a proof-of-concept stems mainly from the unavailability of large-scale, high-velocity test facilities that can accurately simulate the aerocapture environment. In this thesis, several avenues are identified that can bring MAC closer to a successful demonstration of concept feasibility. A custom orbit code that dynamically couples magnetoshell physics with trajectory prop- agation is developed and benchmarked. The code is used to simulate MAC maneuvers for a 60 ton payload at Mars and a 1 ton payload at Neptune, both proposed NASA mis- sions that are not possible with modern flight-ready technology. In both simulations, MAC successfully completes the maneuver and is shown to produce low dynamic pressures and continuously-variable drag characteristics. -
The Meaning of the Constant C in Weber's Electrodynamics
Proe. Int. conf. "Galileo Back in Italy - II" (Soc. Ed. Androme-:ia, Bologna, 2000), pp. 23-36, R. Monti (editor) The Meaning of the Constant c in Weber's Electrodynamics A. K. T. Assis' Instituto de Fisica 'Gleb Wat.aghin' Universidade Estadual de Campinas - Unicamp 13083-970 Campinas, Sao Paulo, Brasil Abstract In this work it is analysed three basic electromagnetic systems of units utilized during last century by Ampere, Gauss, Weber, Maxwell and all the others: The electrostatic, electrodynamic and electromagnetic ones. It is presented how the basic equations of electromagnetism are written in these systems (and also in the present day international system of units MKSA). Then it is shown how the constant c was introduced in physics by Weber's force. It is shown that it has the unit of velocity and is the ratio of the electromagnetic and electrostatic Wlits of charge. Weber and Kohlrausch '5 experiment to determine c is presented, emphasizing that they were 'the first to measure this quantity and obtained the same value as that of light velocity in vacuum. It is shown how Kirchhoff and Weber obtained independently of one another, both working in the framev.-ork of \Veber's electrodynamics, the fact that an electromagnetic signal (of current or potential) propagate at light velocity along a thin wire of negligible resistivity. Key Words: Electromagnetic units, light velocity, wave equation. PACS: O1.55.+b (General physics), 01.65.+g (History of science), 41.20.·q (Electric, magnetic, and electromagnetic fields) ·E-mail: assisOiCLunicamp.br, homepage: www.lCi.unicamp.brrassis AA. VV•. -
Smallsat Aerocapture to Enable a New Paradigm of Planetary Missions
SmallSat Aerocapture to Enable a New Paradigm of Planetary Missions Alex Austin, Adam Nelessen, Bill Ethiraj Venkatapathy, Robin Beck, Robert Braun, Michael Werner, Evan Strauss, Joshua Ravich, Mark Jesick Paul Wercinski, Michael Aftosmis, Roelke Jet Propulsion Laboratory, California Michael Wilder, Gary Allen CU Boulder Institute of Technology NASA Ames Research Center Boulder, CO 80309 Pasadena, CA 91109 Moffett Field, CA 94035 [email protected] 818-393-7521 [email protected] [email protected] Abstract— This paper presents a technology development system requirements, which concluded that mature TPS initiative focused on delivering SmallSats to orbit a variety of materials are adequate for this mission. CFD simulations were bodies using aerocapture. Aerocapture uses the drag of a single used to assess the risk of recontact by the drag skirt during the pass through the atmosphere to capture into orbit instead of jettison event. relying on large quantities of rocket fuel. Using drag modulation flight control, an aerocapture vehicle adjusts its drag area This study has concluded that aerocapture for SmallSats could during atmospheric flight through a single-stage jettison of a be a viable way to increase the delivered mass to Venus and can drag skirt, allowing it to target a particular science orbit in the also be used at other destinations. With increasing interest in presence of atmospheric uncertainties. A team from JPL, NASA SmallSats and the challenges associated with performing orbit Ames, and CU Boulder has worked to address the key insertion burns on small platforms, this technology could enable challenges and determine the feasibility of an aerocapture a new paradigm of planetary science missions. -
Weber's Electrodynamics and the Hall Effect
Weber’s Electrodynamics and the Hall Effect Kirk T. McDonald Joseph Henry Laboratories, Princeton University, Princeton, NJ 08544 (June 5, 2020) 1Problem In 1846, Weber used a model of electric current as moving electric charge (of both signs) to give an instantaneous, action-at-a-distance, “microscopic” force law, from which Amp`ere’s force law between current-carrying circuits could be deduced.1 In Gaussian units, the force on electric charge e due to moving charge e is, according to Weber, 2 ee 2 ∂r r ∂2r Fe,Web er = − 1 − + ˆr, (1) r2 c2 ∂t c2 ∂t2 where r = re −re,andc is the speed of light in vacuum. Following Amp`ere, Weber supposed that the force between two moving charges (current elements) is along their line of centers, and obeys Newton’s third law (of action and reaction). This contrasts with the Lorentz force law, which does not obey Newton’s third law in 2 general, ve e × , Fe,Lorentz = Ee + c Be (2) 3 where the fields Ee and Be are given by the forms of Li´enard and Wiechert. Until the late 1870’s the only experiments possible with electric currents were those in which the currents flowed in complete circuits (as studied by Amp`ere). The first step to- wards a larger context of electric currents was made by Rowland [52, 65] (1876, working in Helmholtz’ lab in Berlin), who showed that a rotating, charged disk produces magnetic effects. More importantly, Rowland’s student Hall (1878) [55] showed that an electric con- ductor in a magnetic field B perpendicular to the current I develops an electric potential 1References to original works are given in the historical Appendix below. -
Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars by Larissa Balestrero Machado a Thesis S
Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars by Larissa Balestrero Machado A thesis submitted to the College of Engineering and Science of Florida Institute of Technology in partial fulfillment of the requirements for the degree of Master of Science in Aerospace Engineering Melbourne, Florida May, 2019 © Copyright 2019 Larissa Balestrero Machado. All Rights Reserved The author grants permission to make single copies ____________________ We the undersigned committee hereby approve the attached thesis, “Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars,” by Larissa Balestrero Machado. _________________________________________________ Markus Wilde, PhD Assistant Professor Department of Aerospace, Physics and Space Sciences _________________________________________________ Andrew Aldrin, PhD Associate Professor School of Arts and Communication _________________________________________________ Brian Kaplinger, PhD Assistant Professor Department of Aerospace, Physics and Space Sciences _________________________________________________ Daniel Batcheldor Professor and Head Department of Aerospace, Physics and Space Sciences Abstract Title: Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars Author: Larissa Balestrero Machado Advisor: Markus Wilde, PhD This thesis presents the results of a conceptual design and aerocapture analysis for a Crew Transfer Vehicle (CTV) designed to carry humans between Earth or Mars and a spacecraft on an Earth-Mars cycler trajectory. The thesis outlines a parametric design model for the Crew Transfer Vehicle and presents concepts for the integration of aerocapture maneuvers within a sustainable cycler architecture. The parametric design study is focused on reducing propellant demand and thus the overall mass of the system and cost of the mission. This is accomplished by using a combination of propulsive and aerodynamic braking for insertion into a low Mars orbit and into a low Earth orbit. -
Lifetime Assessment of the NEXT Ion Thruster
NASA/TM—2010-216915 AIAA–2007–5274 Lifetime Assessment of the NEXT Ion Thruster Jonathan L. Van Noord Glenn Research Center, Cleveland, Ohio November 2010 NASA STI Program . in Profi le Since its founding, NASA has been dedicated to the • CONFERENCE PUBLICATION. Collected advancement of aeronautics and space science. The papers from scientifi c and technical NASA Scientifi c and Technical Information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or cosponsored by NASA. this important role. • SPECIAL PUBLICATION. Scientifi c, The NASA STI Program operates under the auspices technical, or historical information from of the Agency Chief Information Offi cer. It collects, NASA programs, projects, and missions, often organizes, provides for archiving, and disseminates concerned with subjects having substantial NASA’s STI. The NASA STI program provides access public interest. to the NASA Aeronautics and Space Database and its public interface, the NASA Technical Reports • TECHNICAL TRANSLATION. English- Server, thus providing one of the largest collections language translations of foreign scientifi c and of aeronautical and space science STI in the world. technical material pertinent to NASA’s mission. Results are published in both non-NASA channels and by NASA in the NASA STI Report Series, which Specialized services also include creating custom includes the following report types: thesauri, building customized databases, organizing and publishing research results. • TECHNICAL PUBLICATION. Reports of completed research or a major signifi cant phase For more information about the NASA STI of research that present the results of NASA program, see the following: programs and include extensive data or theoretical analysis. -
Unipolar Induction and Weber's Electrodynamics
UNIPOLAR INDUCTION AND WEBER'S ELECTRODYNAMICS Andre K T. Assis,1,2 and Daria S. Thoberl lJnstituto de Fisica 'Gleb Wataghin', Universidade Estadual de Campinas, Unicamp, 13083-970, Campinas, Sao Paulo, Brasil Interneis: [email protected], and [email protected] 2Also Collaborating Professor at the Department of Applied Mathematics, HI/IECe, State University of Campinas, 13083-970 Campinas-SP, Brazil INTRODUCTION Unipolar induction is the generation of current on a conductor for the case 1Il which the conductor and the magnet are in relative rotatory motion. A typical case of unipolar induction is shown in figure 1. ¢ I _galvanometer [--@- and circuit A copper B disk _cylindrical NI permanent I magnet I SI Iaxis Figure 1. Apparatus used to investigate unipolar induction. The sliding contacts in A and B connect the galvanometer to the copper disk. Copper disk and magnet are free to rotate. FronJiers of FundamenJa[ Physics, Edited by M. Barone and F. Selleri, Plenum Press, New York, 1994 409 Since Fara.day's experimcnts L of 18:12 on electromagnetic induction on rotating systems there are intense debates concern ing the loration of the scat of the electromotive force (cmfJ 1 . In this work whenever we speak of "rotation" it should be understood "rotation relative to the earth or laboratory." Let us see what happens in the laboratory. \Vhen we rotate only t.he disk an emf is produced on the galvanometer-disk circuit (the magnet is fixed in the laboratory), as wee can see on the galvanometer. When we rotate only the magnet (the disk is fixed in the laboratory) no current flows by the galvanometer. -
MPD Thruster Technology
NASA Technical Memorandum !05_2_42................................... AIAA-91-3568 p.J_ (NAqA-TM-]05242) MPD T_I&USTER TECHNOLOGY Nqi-32162 ' _f<::_ " _J::_ (NARA) 36 D CSCL 2IH : Unc] dS G3/20 0065762 _ . _,:i;_ _z_ _ :=_: _ MPD Thruster Technology Roger M. Myers Sverdrup Technology, Inc. Lewis Research Center Group Brook Park, Ohio Maris A. Mantenieks National Aeronautics and Space Administration Lewis Research Center := Cleveland, Ohio and Michael R. LaPointe Sverdrup Technology, Inc. Lewis Research Center Group Brook Park, Ohio _= P.repared for the ..... Conference on Adyanced Space Exploration Initiative Techn6logies cosponsored by AIAA, NASA, and OAI Cleveland, Ohio, September 4-6, 1991 RI/ A MPD Thruster Technology Roger M. Myers Sverdrup Technology, Inc. NASA Lewis Research Center Group Brook Park, OH 44142 Marls A. Mantenieks NASA Lewis Research Center Cleveland, OH 44135 Michael R. l.atPointe Sverdrup Technology, Inc. NASA Lewis Research Center Group Brook Park, OH 44142 Abstract MPD thrusters have demonstrated between 2000 and 7000 seconds specific impulse at efficiencies approaching 40 %, and have been operated continuously at power levels over 500 kW. These demonstrated capabilities, combined with the simplicity and robustness of the thruster, make them attractive candidates for application to both unmanned and manned orbit raising, lunar, and planetary missions. To date, however, only a limited number of thruster confiurations, propellants, and operating conditions have been studied. This work reviews the present status of MPD thruster research, including developments in the _ performance levels and electrode erosion rates, and theoretical studies of the thruster dynamics. Significant progress has been made in establishing empirical scaling laws, performance and lifetime limitations and in the development of numerical codes to simulate the flow field and electrode processes. -
Magnetoplasmadynamic Thruster with an Applied Field Based on the Second Generation High-Temperature Superconductors
Journal of Physics: Conference Series PAPER • OPEN ACCESS Magnetoplasmadynamic thruster with an applied field based on the second generation high-temperature superconductors To cite this article: A.S. Voronov et al 2020 J. Phys.: Conf. Ser. 1686 012023 View the article online for updates and enhancements. This content was downloaded from IP address 170.106.35.93 on 26/09/2021 at 09:02 LaPlas 2020 IOP Publishing Journal of Physics: Conference Series 1686 (2020) 012023 doi:10.1088/1742-6596/1686/1/012023 Magnetoplasmadynamic thruster with an applied field based on the second generation high-temperature superconductors A.S. Voronov1, A.A. Troitskiy1, I.D. Egorov2, S.V. Samoilenkov1, A.P. Vavilov1 1 Сlosed Joint Stock Company «SuperOx», Moscow, Russia 2 National Research Nuclear University «MEPhI», Moscow, Russia E-mail: [email protected] Abstract. The present work reports the results of the magnetoplasmadynamic (MPD) thruster with an applied field (AF) based on the second-generation high-temperature superconductor (2G HTS) tape functioning research. Achieved thrust, specific impulse, and efficiency were investigated. Experiments were performed on the 25-kW magnetoplasmadynamic thruster model with two types of 10-mm and 17-mm cathodes. The investigation tests were performed with the goal of studying the efficiency of using 2G HTS tape as electromagnetic coils creating applied field for MPD thruster. The used as the applied magnetic field for thruster 2G HTS coil creates magnetic field up to 1 Tesla. The results showed that the thrust and specific impulse with HTSC applied field increases up to 300% and efficiency increases up to 700%. -
Comparison Between Weber's Electrodynamics and Classical Electrodynamics
PRAMANA c Indian Academy of Sciences Vol. 55, No. 3 — journal of September 2000 physics pp. 393–404 Comparison between Weber’s electrodynamics and classical electrodynamics A K T ASSIS £ and H TORRES SILVA Facultad de Ingenieria, Universidad de Tarapaca, Av. 18 de Septiembre 2222, Arica, Chile £ Permanent address: Instituto de F´ısica ‘Gleb Wataghin’, Universidade Estadual de Campinas - Unicamp, 13083-970 Campinas, S˜ao Paulo, Brasil Email: [email protected]; [email protected] MS received 20 January 2000; revised 25 April 2000 Abstract. We present the main aspects of Weber’s electrodynamics and of Maxwell’s equations. We discuss Maxwell’s point of view related to Weber’s electrodynamics. We compare Weber’s force with Lorentz’s force. We analyse the relation between Weber’s law and Maxwell’s equations. Finally, we discuss some experiments performed and proposed with which we can distinguish Weber’s force from Lorentz’s one. Keywords. Weber’s electrodynamics; Maxwell’s equations; Lorentz’s force; classical electromag- netism. PACS Nos 41.20.Bt; 41.20.-q; 03.50.De 1. Weber’s electrodynamics Wilhelm Weber (1804–1891) developed his electrodynamics during the same period in which James Clerk Maxwell (1831–1879) was putting together what are known as Maxwell’s equations. In this work we compare these two electrodynamics. We begin presenting the main aspects of Weber’s electrodynamics. For complete ref- Õ ~Ö ¾ erences, see [1] and [2]. Suppose we have a point charge ¾ located on relative to the Ë ~Ú ~a ¾ origin of an inertial frame of reference , moving with velocity ¾ and acceleration , Õ ~Ö ~Ú ~a ½ ½ ½ and another point charge ½ located on and moving with velocity and acceleration relative to Ë . -
The Short History of Science
PHYSICS FOUNDATIONS SOCIETY THE FINNISH SOCIETY FOR NATURAL PHILOSOPHY PHYSICS FOUNDATIONS SOCIETY THE FINNISH SOCIETY FOR www.physicsfoundations.org NATURAL PHILOSOPHY www.lfs.fi Dr. Suntola’s “The Short History of Science” shows fascinating competence in its constructively critical in-depth exploration of the long path that the pioneers of metaphysics and empirical science have followed in building up our present understanding of physical reality. The book is made unique by the author’s perspective. He reflects the historical path to his Dynamic Universe theory that opens an unparalleled perspective to a deeper understanding of the harmony in nature – to click the pieces of the puzzle into their places. The book opens a unique possibility for the reader to make his own evaluation of the postulates behind our present understanding of reality. – Tarja Kallio-Tamminen, PhD, theoretical philosophy, MSc, high energy physics The book gives an exceptionally interesting perspective on the history of science and the development paths that have led to our scientific picture of physical reality. As a philosophical question, the reader may conclude how much the development has been directed by coincidences, and whether the picture of reality would have been different if another path had been chosen. – Heikki Sipilä, PhD, nuclear physics Would other routes have been chosen, if all modern experiments had been available to the early scientists? This is an excellent book for a guided scientific tour challenging the reader to an in-depth consideration of the choices made. – Ari Lehto, PhD, physics Tuomo Suntola, PhD in Electron Physics at Helsinki University of Technology (1971).