Phenomenology of the Lense-Thirring Effect in the Solar System
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Phase Transition of Quantum-Corrected Schwarzschild Black Hole in Rainbow Gravity
Physics Letters B 784 (2018) 6–11 Contents lists available at ScienceDirect Physics Letters B www.elsevier.com/locate/physletb Phase transition of quantum-corrected Schwarzschild black hole in rainbow gravity Md. Shahjalal Department of Mathematics, Shahjalal University of Science and Technology, Sylhet-3114, Bangladesh a r t i c l e i n f o a b s t r a c t Article history: The thermodynamic phase transition of Schwarzschild black hole, after employing a quantum correction Received 30 May 2018 to the space–time metric, in the gravity’s rainbow is explored. The rainbow gravity-inspired Hawking Received in revised form 15 July 2018 temperature of the quantum-corrected rainbow Schwarzschild black hole is calculated initially, and then Accepted 16 July 2018 the entropy, the local temperature, and the local energy of the black hole in an isothermal cavity Available online 20 July 2018 are derived. The off-shell free energy is calculated to further investigate the critical behavior, the Editor: B. Grinstein thermodynamic stability, and the phase transition of the black hole. It is evident that the rainbow gravity Keywords: determines the late fate of the black hole as leading to a remnant, the findings of this letter also show Rainbow gravity that a quantum correction to the metric reduces the remnant mass of the Schwarzschild black hole in Black hole thermodynamics comparison with the usual rainbow Schwarzschild black hole. Phase transition © 2018 The Author(s). Published by Elsevier B.V. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/). -
Analysis of Planetary and Solar-Induced Perturbations on Trans-Martian Trajectory of Mars Missions Before and After Mars Orbit Insertion
Analysis of planetary and solar-induced perturbations on trans-Martian trajectory of Mars missions before and after Mars orbit insertion V U J Nwankwo1 and S K Chakrabarti1,2* 1S N Bose National Centre for Basic Sciences, Kolkata 700 098, West Bengal, India 2Indian Center for Space Physics, Kolkata 700 084, West Bengal, India Abstract: Interplanetary missions are susceptible to gravitational and nongravitational perturbing forces at every tra- jectory phase, assuming, of course, that the man made rockets and thrusters work as expected. These forces are mainly due to planetary and solar-forcing-induced perturbations during geocentric, heliocentric and Martian trajectories, and before orbit insertion. In this study, we review and/or analyze Mars orbiters mission associated perturbing forces and their possible impacts before Mars Orbit Insertion viz Earth’s oblateness, Third body (solar and lunar), solar radiation pressure, solar energetic radiation environment and atmospheric drag forces. We also model the significance of atmospheric drag force on Mangalyaan Mars orbiter mission, as a function of appropriate space environmental parameters during its 28 days in Earth’s orbit (around and during perigee passage), 300 days of heliocentric and 100 days of Martian trajectory. We have found that for a total perigee height boost of about 250 km, the cumulative orbit decay can be approximately 720 m. The approximate altitude variation could be up to 158 m with respect to the sun during 300 days of interplanetary journey toward Mars. After Mars orbit insertion, the total decay experienced by the spacecraft could be up to 701 m with decay rate of up to 9 m/day during 100 days of Martian trajectory, based on Mars–Earth atmosphere density ratio. -
Field Theory Aspects of Cosmology and Black Holes
FIELD THEORY ASPECTS OF COSMOLOGY AND BLACK HOLES Thesis submitted for the degree of Doctor of Philosophy (Science) of Jadavpur University, Kolkata August 2009 arXiv:1011.6570v1 [hep-th] 30 Nov 2010 Kulkarni Shailesh Gajanan Satyendra Nath Bose National Centre for Basic Sciences JD Block, Sector 3, Salt Lake, Kolkata 700098, India Certificate from the supervisor This is to certify that the thesis entitled \Field theory aspects of cosmology and black holes" submitted by Sri. Kulkarni Shailesh Gajanan, who got his name registered on October 8, 2007 for the award of Ph.D. (Science) degree of Jadavpur University, is absolutely based upon his own work under the supervision of Professor Rabin Banerjee at S.N. Bose National Centre for Basic Sciences, Kolkata, India, and that neither this thesis nor any part of it has been submitted for any degree/diploma or any other academic award anywhere before. Rabin Banerjee Professor S.N. Bose National Centre for Basic Sciences JD Block, Sector 3, Salt Lake Kolkata 700098, India TO MY MOT HER Acknowledgements This thesis is the culminative outcome of five years work, which has been made possible by the blessings and support of many individuals. I take this opportunity to express my sincere gratitude to all of them. First and foremost, I would like to thank Prof. Rabin Banerjee, my thesis supervisor. His uncanny ability to select a particular problem, a keen and strategic analysis of it and deep involvement among the students makes him something special. Thank you Sir for giving me all that could last my entire life. -
Theoretical and Experimental Investigation of Hall Thruster Miniaturization by Noah Zachary Warner
Theoretical and Experimental Investigation of Hall Thruster Miniaturization by Noah Zachary Warner S.B., Aeronautics and Astronautics, Massachusetts Institute of Technology, 2001 S.M., Aeronautics and Astronautics, Massachusetts Institute of Technology, 2003 SUBMITTED TO THE DEPARTMENT OF AERONAUTICS AND ASTRONAUTICS IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF PHILOSOPHY AT THE MASSACHUSETTS INSTITUTE OF TECHNOLOGY JUNE 2007 © 2007 Massachusetts Institute of Technology. All rights reserved. Signature of Author . Department of Aeronautics and Astronautics May 25, 2007 Certified by . Manuel Martínez-Sánchez Professor of Aeronautics and Astronautics Thesis Supervisor Certified by . Jack Kerrebrock Professor Emeritus of Aeronautics and Astronautics Certified by . Oleg Batishchev Principal Research Scientist in Aeronautics and Astronautics Certified by . Vladimir Hruby President, Busek Company, Inc. Accepted by . Jaime Peraire Professor of Aeronautics and Astronautics Chair, Committee on Graduate Students 2 Theoretical and Experimental Investigation of Hall Thruster Miniaturization by Noah Zachary Warner Submitted to the Department of Aeronautics and Astronautics on May 25, 2007 in partial fulfillment of the requirements for the degree of Doctor of Philosophy in Aeronautics and Astronautics in the field of Space Propulsion ABSTRACT Interest in small-scale space propulsion continues to grow with the increasing number of small satellite missions, particularly in the area of formation flight. Miniaturized Hall thrusters have been identified as a candidate for lightweight, high specific impulse propul- sion systems that can extend mission lifetime and payload capability. A set of scaling laws was developed that allows the dimensions and operating parameters of a miniaturized Hall thruster to be determined from an existing, technologically mature baseline design. -
Earth to Mars Areostationary Mission Optimization Analysis
Earth to Mars areostationary mission optimization analysis M. M. Sánchez-García, G. Barderas and P. Romero Instituto de Matemática Interdisciplinar. U. D. Astronomía y Geodesia, Facultad de Ciencias Matemáticas, Universidad Complutense de Madrid, Madrid, Spain ([email protected], [email protected], [email protected]) Abstract Mars has become one of the priorities in the planetary exploration programs. The analysis of space mission costs has become a key factor in mission planning. The determination of optimal trajectories aiming to lower costs in terms of impulses allows for more massive payloads to be transported at a minimum energy cost. Areostationary satellites are considered the most efficient and robust candidates to satisfy the control needs of the missions to Mars. Mars Areostationary Relay Satellites providing continuous coverage of a specific region of Mars are being considered for a near future. In this work, we analyze the optimization of an areostationary mission. We first determine the launch and arrival dates for an optimal minimum energy Earth-Mars transfer trajectory. Then, the minimum thrust maneuvers to capture the spacecraft from the hyperbolic arrival trajectory to Mars and place it in the areostationary orbit are analyzed. XIV.0 Reunión Científica 13-15 julio 2020 Context of the research: Previous studies The number of missions to Mars has increased over the last years, particularly robotic missions which need to be tele- commanded from the Earth. The need to control the different missions in Mars in almost real time with a relay system that provides continuous coverage of a specific region has been proposed by several authors such as Edwards et al. -
Quantum Wave Mechanics 3Rd Ed
Geometrical description of photons, electrons and composite particles. Dimensional analysis of electrical charge. Quantum gravity, gravitational frequency spectrum, mass oscillator synchronization, spectral energy density modulation and phase conjugation. Origin of charge, fine structure constant and inertia. Prospects for wave-based EM propulsion. Quantum Wave Mechanics by Larry Reed Order the complete book from the publisher Booklocker.com https://www.booklocker.com/p/books/10176.html?s=pdf or from your favorite neighborhood or online bookstore. To my parents who never knew the result of their great experiment Copyright © 2019, 2020 by Larry J. Reed All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted in any form or by any means, electronic, mechanical, recording or otherwise, without the prior written permission of the author. Printed on acid-free paper. Library of Congress Control Number: 2018901065 ISBN: 978-1-63492-964-6 paperback To order additional copies of this book, contact: www.booklocker.com CONTENTS Preface ........................................................................................................................... ix SECTION 1 – LIGHT 1. Photon model ................................................................................................................. 1 2. Quantum vacuum ......................................................................................................... 13 3. Electromagnetic 4-Potential ....................................................................................... -
'.';King Navigation
1980012912 -' JPL PUBLICATION 78-38 '.';king Navigation W. J. O'Neil, R. P. Rudd, D. L. Farless, C. E. Hildebrand, R. T. Mitchell, K. H. Rourke, et al. Jet Propulsion Laboratory E. A. Euler Martin Marietta Aerospace (N,%SA-C[_-l_,2517) VIklt_G ._AVIGA'IION (Jet t, u0-213_-_ : Pcopulsio[, L,_c.) 322 p _lC Alq/MF A01 _:d[,U CSCL Z2.t; hd0-_|4dj •_ [J_;c ]. a_ GJ/15 l,t7 5 'JJ ± November 15, 1979 _',r:.'> ;Y/l&_',,/I_cC7.'/',_/, : < X* ",t ,'" t National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California # 1980012912-002 JPL PUBLICATION 78-38 Viking Navigation W. J. O'Neil, R. P. Rudd, D. L. Farless, C. E. Hildebrand, R. T. Mitchell, K. H. Rourke, et al. Jet Propulsion Laboratory E. A. Euler Martin Marietta Aerospace November 15, 1979 National Aeronautics and Space Administration Jet Propulsion Laboratory : California Institute of Technology Pasadena, California 1980012912-003 The research descnbed bnth_s pubhcat_onwas camed out by the Jet Propulsion Laboratory, Cahforn_aInstitute of Technology, under NASA Contract No NAS7-100 i 1980012912-004 Abstract NASA soft-landed two Viking spacecraft on Mars in the summer t,f 1976. These were the free world's first landings on another planet. This report provides a final, comprehensive description of the navigation of the Viking spacecraft throughout their flight from Earth launch to Mars landing. The flight path design, actual int]lght control, and postflight reconstruction ale discussed in detail. The report Is comprised of an introductory chapter followed by five Olapters which essenually correspond to the organization of the Viking navigation operations, namely, Trajectory Descriptton, Interplanetary Orbit Determination, Satellite Orbit Determination, ._haneuver Analysis, and Lander Flight Path Analysis. -
An Access-Dictionary of Internationalist High Tech Latinate English
An Access-Dictionary of Internationalist High Tech Latinate English Excerpted from Word Power, Public Speaking Confidence, and Dictionary-Based Learning, Copyright © 2007 by Robert Oliphant, columnist, Education News Author of The Latin-Old English Glossary in British Museum MS 3376 (Mouton, 1966) and A Piano for Mrs. Cimino (Prentice Hall, 1980) INTRODUCTION Strictly speaking, this is simply a list of technical terms: 30,680 of them presented in an alphabetical sequence of 52 professional subject fields ranging from Aeronautics to Zoology. Practically considered, though, every item on the list can be quickly accessed in the Random House Webster’s Unabridged Dictionary (RHU), updated second edition of 2007, or in its CD – ROM WordGenius® version. So what’s here is actually an in-depth learning tool for mastering the basic vocabularies of what today can fairly be called American-Pronunciation Internationalist High Tech Latinate English. Dictionary authority. This list, by virtue of its dictionary link, has far more authority than a conventional professional-subject glossary, even the one offered online by the University of Maryland Medical Center. American dictionaries, after all, have always assigned their technical terms to professional experts in specific fields, identified those experts in print, and in effect held them responsible for the accuracy and comprehensiveness of each entry. Even more important, the entries themselves offer learners a complete sketch of each target word (headword). Memorization. For professionals, memorization is a basic career requirement. Any physician will tell you how much of it is called for in medical school and how hard it is, thanks to thousands of strange, exotic shapes like <myocardium> that have to be taken apart in the mind and reassembled like pieces of an unpronounceable jigsaw puzzle. -
Back Reaction, Covariant Anomaly and Effective Action
Preprint typeset in JHEP style - HYPER VERSION Back reaction, covariant anomaly and effective action Qing-Quan Jianga,b and Xu Caib a Institute of Theoretical Physics, China West Normal University, Nanchong, Sichuan 637002, People’s Republic of China b Institute of Particle Physics, Central China Normal University, Wuhan, Hubei 430079, People’s Republic of China E-mail address: [email protected], [email protected] Abstract: In the presence of back reaction, we first produce the one-loop corrections for the event horizon and Hawking temperature of the Reissner-Nordstr¨om black hole. Then, based on the covariant anomaly cancelation method and the effective action technique, the modified expressions for the fluxes of gauge current and energy momentum tensor, due to the effect of back reaction, are obtained. The results are consistent with the Hawking fluxes of a (1+1)-dimensional blackbody at the temperature with quantum corrections, thus confirming the robustness of the covariant anomaly cancelation method and the effective action technique for black holes with back reaction. arXiv:1005.0999v1 [gr-qc] 6 May 2010 Keywords: Black holes, Modes of Quantum Gravity. Contents 1. Introduction 1 2. Back reaction on the Reissner-Nordstr¨om black hole 2 3. Back reaction and covariant anomalies 4 4. Back reaction and effective action 7 5. Conclusions and discussions 9 A. Dimensional analysis 11 1. Introduction Hawking proved that black holes are not perfectly black, rather they can radiate particles characterized by the thermal spectrum with the temperature T = (1/2π)κ, where κ is the surface gravity of the black hole[1]. -
Metaphorizing Dialogue to Enact a Flow Culture Transcending Divisiveness by Systematic Embodiment of Metaphor in Discourse -- /
Alternative view of segmented documents via Kairos 6 May 2019 | Draft Metaphorizing Dialogue to Enact a Flow Culture Transcending divisiveness by systematic embodiment of metaphor in discourse -- / -- Introduction Metaphorizing -- beyond one-off usage Sustaining dialogue through metaphor? Indicative precedents of metaphorizing skills Discourse and debate reframed as cognitive combat through metaphor? Integrity of metaphorizing framed by complementarity between alternatives Imagining a relevant philosophers' game -- and beyond Requisite metaphoric "circumlocution" avoiding disruptive disagreement Sustainable discourse framed metaphorically as "orbiting" Metaphorizing as artful indulgence in misplaced concreteness? Re-imagining: metaphorizing, metamorphizing and cognitive shapeshifting Sustainable discourse: longest conflict versus longest conversation? References Introduction There is no difficulty in recognizing the extent to which discourse has become problematic, whether in national assemblies, parliaments, or the media (social media or otherwise). The current scene has been described as poisonously divisive. Each faction is adamant that the facts and principles it presents are beyond question. Each is necessarily right, with any in disagreement being by definition wrong. Discourse between nations, between religions, between political parties, and between disciplines currently offers little hope for a more fruitful modality. Curiously efforts towards transcending this situation -- if they are more than tokenistic -- seem to be readily entrapped by the same dynamic. Each is necessarily right or better, with others essentially misguided, misinformed or behind the times. The following is an exploration of a distinctive mode which does not rely on facts and truth as commonly understood, or on the deprecation of fake news and pretence. The focus is not on being right or wrong or the attribution of blame. -
Astronomy and Astrophysics
A Problem book in Astronomy and Astrophysics Compilation of problems from International Olympiad in Astronomy and Astrophysics (2007-2012) Edited by: Aniket Sule on behalf of IOAA international board July 23, 2013 ii Copyright ©2007-2012 International Olympiad on Astronomy and Astrophysics (IOAA). All rights reserved. This compilation can be redistributed or translated freely for educational purpose in a non-commercial manner, with customary acknowledgement of IOAA. Original Problems by: academic committees of IOAAs held at: – Thailand (2007) – Indonesia (2008) – Iran (2009) – China (2010) – Poland (2011) – Brazil (2012) Compiled and Edited by: Aniket Sule Homi Bhabha Centre for Science Education Tata Institute of Fundamental Research V. N. Purav Road, Mankhurd, Mumbai, 400088, INDIA Contact: [email protected] Thank you! Editor would like to thank International Board of International Olympiad on Astronomy and Astrophysics (IOAA) and particularly, president of the board, Prof. Chatief Kunjaya, and general secretary, Prof. Gregorz Stachowaski, for entrusting this task to him. We acknowledge the hard work done by respec- tive year’s problem setters drawn from the host countries in designing the problems and fact that all the host countries of IOAA graciously agreed to permit use of the problems, for this book. All the members of the interna- tional board IOAA are thanked for their support and suggestions. All IOAA participants are thanked for their ingenious solutions for the problems some of which you will see in this book. iv Thank you! A Note about Problems You will find a code in bracket after each problem e.g. (I07 - T20 - C). The first number simply gives the year in which this problem was posed I07 means IOAA2007. -
Performance Testing and Internal Probe Measurements of a High Specific Impulse Hall Thruster
Performance Testing and Internal Probe Measurements of a High Specific Impulse Hall Thruster by Noah Zachary Warner S.B., Aeronautics and Astronautics Massachusetts Institute of Technology, 2001 Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY September 2003 © 2003 Massachusetts Institute of Technology. All rights reserved. Signature of Author . Department of Aeronautics and Astronautics August 5, 2003 Certified by . Manuel Martinez-Sanchez Professor of Aeronautics and Astronautics Thesis Supervisor Accepted by . Edward M. Greitzer H.N. Slater Professor of Aeronautics and Astronautics Chair, Committee on Graduate Students 2 Performance Testing and Internal Probe Measurements of a High Specific Impulse Hall Thruster by Noah Zachary Warner Submitted to the Department of Aeronautics and Astronautics on August 5, 2003 in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics ABSTRACT The BHT-1000 high specific impulse Hall thruster was used for performance testing and internal plasma measurements to support the ongoing development of computational mod- els. The thruster was performance tested in both single and two stage anode configura- tions. In the single stage configuration, the specific impulse exceeded 3000s at a discharge voltage of 1000V while maintaining a thrust efficiency of 50 percent. Two stage operation produced higher thrust, specific impulse and thrust efficiency than the single stage configuration at most discharge voltages. The thruster thermal warmup was charac- terized using a thermocouple embedded in the outer exit ring, and the magnetic field topology was investigated using a Gaussmeter.