UC Davis UC Davis Previously Published Works
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Hawking Radiation
a brief history of andreas müller student seminar theory group max camenzind lsw heidelberg mpia & lsw january 2004 http://www.lsw.uni-heidelberg.de/users/amueller talktalk organisationorganisation basics ☺ standard knowledge advanced knowledge edge of knowledge and verifiability mindmind mapmap whatwhat isis aa blackblack hole?hole? black escape velocity c hole singularity in space-time notion „black hole“ from relativist john archibald wheeler (1968), but first speculation from geologist and astronomer john michell (1783) ☺ blackblack holesholes inin relativityrelativity solutions of the vacuum field equations of einsteins general relativity (1915) Gµν = 0 some history: schwarzschild 1916 (static, neutral) reissner-nordstrøm 1918 (static, electrically charged) kerr 1963 (rotating, neutral) kerr-newman 1965 (rotating, charged) all are petrov type-d space-times plug-in metric gµν to verify solution ;-) ☺ black hole mass hidden in (point or ring) singularity blackblack holesholes havehave nono hairhair!! schwarzschild {M} reissner-nordstrom {M,Q} kerr {M,a} kerr-newman {M,a,Q} wheeler: no-hair theorem ☺ blackblack holesholes –– schwarzschildschwarzschild vs.vs. kerrkerr ☺ blackblack holesholes –– kerrkerr inin boyerboyer--lindquistlindquist black hole mass M spin parameter a lapse function delta potential generalized radius sigma potential frame-dragging frequency cylindrical radius blackblack holehole topologytopology blackblack holehole –– characteristiccharacteristic radiiradii G = M = c = 1 blackblack holehole -- -
A Search for an Additional Planet in the Hot-Jupiter System WASP-5 by Transit Timing Variations
A Search for an Additional Planet in the Hot-Jupiter System WASP-5 by Transit Timing Variations Akihiko Fukui Division of Particle and Astrophysical Science, Graduate School of Science, Nagoya University July 19, 2011 Abstract Searching for transit timing variations (TTVs) of a transiting extrasolar planet can be a tool to ¯nd additional, even less massive planets existing in the same system. In addition, such additional-planet searches around hot Jupiters can be a test for migration mechanisms of hot Jupiters. We observed 7 new transits of the hot Jupiter WASP-5b by using a 61 cm telescope located in New Zealand, aiming for detecting TTVs induced by an additional planet. When combined with other available photometric and radial velocity (RV) data, we ¯nd that its transit timings do not match a linear ephemeris; the best ¯t Â2 values is 32.2 with 9 degrees of freedom, which corresponds to a con¯dence level of 99.982 % or 3.7 σ. Considering possible imperfect corrections of light-curve baselines, the Â2 value reduces to 24.7, which corresponds to a con¯dence level of 99.668 % or 2.9 σ. From the absence of signi¯cant TTV signals, we calculate upper limits of the mass of an hypothetical additional planet by means of numerical simulations, as a function of orbital-period ratio of the two planets. We place the limits of 2 M© (3 σ conf.) near 1:2 and 2:1 mean motion resonances (MMRs) with WASP-5b, assuming that the two planets are co-planer. These limits narrow the limits placed from the RV data only, where the limits of 22-70 M© over the orbital-period ratio from 0.2 to 5.0 are placed. -
8.901 Lecture Notes Astrophysics I, Spring 2019
8.901 Lecture Notes Astrophysics I, Spring 2019 I.J.M. Crossfield (with S. Hughes and E. Mills)* MIT 6th February, 2019 – 15th May, 2019 Contents 1 Introduction to Astronomy and Astrophysics 6 2 The Two-Body Problem and Kepler’s Laws 10 3 The Two-Body Problem, Continued 14 4 Binary Systems 21 4.1 Empirical Facts about binaries................... 21 4.2 Parameterization of Binary Orbits................. 21 4.3 Binary Observations......................... 22 5 Gravitational Waves 25 5.1 Gravitational Radiation........................ 27 5.2 Practical Effects............................ 28 6 Radiation 30 6.1 Radiation from Space......................... 30 6.2 Conservation of Specific Intensity................. 33 6.3 Blackbody Radiation......................... 36 6.4 Radiation, Luminosity, and Temperature............. 37 7 Radiative Transfer 38 7.1 The Equation of Radiative Transfer................. 38 7.2 Solutions to the Radiative Transfer Equation........... 40 7.3 Kirchhoff’s Laws........................... 41 8 Stellar Classification, Spectra, and Some Thermodynamics 44 8.1 Classification.............................. 44 8.2 Thermodynamic Equilibrium.................... 46 8.3 Local Thermodynamic Equilibrium................ 47 8.4 Stellar Lines and Atomic Populations............... 48 *[email protected] 1 Contents 8.5 The Saha Equation.......................... 48 9 Stellar Atmospheres 54 9.1 The Plane-parallel Approximation................. 54 9.2 Gray Atmosphere........................... 56 9.3 The Eddington Approximation................... 59 9.4 Frequency-Dependent Quantities.................. 61 9.5 Opacities................................ 62 10 Timescales in Stellar Interiors 67 10.1 Photon collisions with matter.................... 67 10.2 Gravity and the free-fall timescale................. 68 10.3 The sound-crossing time....................... 71 10.4 Radiation transport.......................... 72 10.5 Thermal (Kelvin-Helmholtz) timescale............... 72 10.6 Nuclear timescale.......................... -
Nasa.Gov/Search.Jsp?R=19940022855 2020-06-16T13:30:04+00:00Z
https://ntrs.nasa.gov/search.jsp?R=19940022855 2020-06-16T13:30:04+00:00Z NASA Conference Publication 10129 Vision-21 Interdisciplinary Science and Engineering in the Era of Cyberspace Proceedings of a symposium cosponsored by the NASA Lewis Research Center and the Ohio Aerospace Institute and held in Westlake, Ohio March 30-31, 1993 (NASA-CP-IOI2Q) VISION 21: N94-27358 INTERDISCIPLINARY SCIENCE AND --THRU-- m ENGINEERING IN THE ERA OF N94-27376 CY_ERSPACE (NASA) 274 p Uncl as I IASA G3/12 0206714 NASA Conference Publication 10129 Vision-21 Interdisciplinary Science and Engineering in the Era of Cyberspace Proceedings of a symposium cosponsored by the NASA Lewis Research Center and the Ohio Aerospace Institute and held in Westlake, Ohio March 30-31, 1993 NASA National Aeronautics and Space Administration Office of Management Scientific and Technical Information Program 1993 Into the Era of Cyberspace Our robots precede us with infinite diversity exploring the universe delighting in complexity A matrix of neurons, we create our own reality of carbon and of silicon, we evolve toward what we chose to be. GL 1993 iii PilIJl)I4_$ PAG[ I!ILA!'_I(. NOT _t__O FOREWORD The symposium "Vision 21: Interdisciplinary Science and Engineering in the Era of Cyberspace" was held at the Holiday Inn in Westlake, Ohio on March 30-31, 1993, sponsored by the NASA Lewis Research Center's Aerospace Technology Directorate under the auspices of the NASA Office of Aeronautics, Exploration and Technology. In the NASA space program there is always a major focus on near-term development of technologies and hardware; however, there is also a continuing need to consider the more visionary far-term concepts and ideas that might lead to radical breakthroughs in the next century. -
PHASEA ~ORT(REVISED) a IVIAN-CCMPUTER ROLES in SPACE NAVIGATION and GUIDANCE
PHASEA ~ORT(REVISED) a IVIAN-CCMPUTER ROLES IN SPACE NAVIGATION AND GUIDANCE , '' Eugene Farber The Frank1 in Institute Research Laboratories and Lloyd P. Crumley and Lou Spiegel . General Electric Company January 18, 1967 \ prepared for Electronics Research Center Cambridge National Aeronautics and Space Administration under contract number NAS 12-128 i INSlTUTE RESEARCH LABORATORES 1 I SYSTEMS SCIENCE DIVISION This report is a revision of the Phase I report submitted to NASA by The Franklin Institute Re- search Laboratories on October 17, 1966, and is submitted in accordance with the requirements of contract NAS 12-128. Approved: Carl A. Silver Manager Behavioral Sciences Laboratory 0 4 E e TABLE OF CONTENTS 1 Section Title Page 1 SECTION 1. INTRODUCTION ...................... 1-1 SECTION 2 . MISSION DESCRIPTION 2.1 . General Mission Constraints ................ 2-1 8 2.5 . Navigation and Guidanoe Events .............. 2-7 SECTION 3. NAVIGATION AND GUIDANCE PHASE DESCRIPTIONS E 3.1. Earth Cycle. Part 1 .................... 3-1 3.5 Interplanetary Cycle ................... 3-3 3.22 . Earth Cycle. Part 2 .................... 3-6 1 3.26. Mars Cycle ........................ 3-6 3.32. Classification of Phases by hotion ........... 3-7 8 3.33 . Functions Deleted from Consideration ........... 3-7 SECTION 4. ERROR-SENSITIVITY ANALYSIS 4.1 . Injection ......................... 4-2 8 4.6 . Post and Terminal Adjustments ............... 4-11 4.7 . Orbit Errtry. ....................... 4-15 8 4.0 . summsry .......................... 4-18 SECTION 5 . NAVIGATION AND GUIDANCE 5.1 . Orbit Determination. ................... 5-1 1 5.6 . Injection ......................... 5-8 5.9 . Post and Terminal Adjustment ............... 5-17 5.13 . Orbit Entry ........................ 5-26 I 5.16 . -
Radiatively Driven Stellar Winds from Hot Stars E NCYCLOPEDIA of a STRONOMY and a STROPHYSICS
Radiatively Driven Stellar Winds from Hot Stars E NCYCLOPEDIA OF A STRONOMY AND A STROPHYSICS Radiatively Driven Stellar Winds from strong convection zone needed to heat a circumstellar corona. Their stellar winds thus remain at temperatures Hot Stars comparable with the star’s surface, and so lack the very A stellar wind is the continuous, supersonic outflow of high gas pressure needed to drive an outward expansion matter from a star. Among the most massive stars—which against the stellar gravity. However, such hot stars tend also to be the hottest and most luminous—the winds have a quite high radiative flux, since by the Stefan– can be very strong, with important consequences both for Boltzmann law this scales as the fourth power of the the star’s own evolution as well as for the surrounding surface temperature. It is the pressure of this radiation (not interstellar medium. Such hot-star winds are understood of the gas itself) that drives the wind expansion. to be driven by the pressure of the star’s emitted radiation. The typical flow speeds of hot-star winds—up to −1 Our Sun has a SOLAR WIND, but it is so tenuous and about 3000 km s —are a factor of a few faster than the 400– −1 transparent that it would be difficult to detect directly from 700 km s speed of the solar wind. However, the inferred a more distant star. However, many stars have winds that mass loss rates of hot stars greatly exceed—by up to a factor are dense enough to be opaque at certain wavelengths of a billion—that of the Sun. -
Starship Size Table
My Spacedock construction notes all it there are some other peoples stuff in here but not all has credits to it. This is just my notes and I saw that there was interest out there in it so I generated a PDF for everyone who wants to use it. Omerga1967 Spacedock New & Alternative Tech from the net These notes from the web for Spacedock are useful and have significant purpose. I have used only a few in modifications but keep a copy of them with the pages of the Spacedock that I have printed in the use of constructing starships and space stations. STARSHIP SIZE TABLE Starship Space Length Beam Height SU Mass Range Size Station + 2,000 m + 2,000 m +2,0 00 m +3,000 – 6,000 +10 ,000,000 to 20,000,000 metric tonnes 50 13 72,000 – 73,999 68,000 – 69,999 m 60,000 - 61,999 m 107,000 –193,000 310,000,000 – 519,999,999 metric tonnes 49 13 70,000 – 71,999 m 66,000 – 67,999 m 58,000 - 59,999 m 104,000 –187,000 300,000,000 – 499,999,999 metric tonnes 48 12 68,000 – 69,999 m 64,000 – 65,999 m 56,000 - 57,999 m 101,000 – 181,000 290,000,000 - 479,999,999 met ric tonnes 47 12 66,000 – 67,999 m 62,000 – 63,999 m 54,000 - 55,999 m 98,000 – 175,000 280,000,000 – 459,999,999 metric tonnes 46 12 64,000 – 65,999 m 60,000 – 61,999 m 52,000 - 53,999 m 95,000 –169,000 270,000,000 – 439,999,999 metric tonnes 45 12 62, 000 – 63,999 m 58,000 – 59,999 m 50,000 - 51,999 m 92,000 –163,000 260,000,000 – 419,999,999 metric tonnes 44 11 60,000 – 61,999 m 56,000 – 57,999 m 48,000 - 49,999 m 89,000 – 157,000 250,000,000 – 399,999,999 metric tonnes 43 11 58,000 – 59,999 m 54,00 -