Librational Response of Europa, Ganymede, and Callisto with an Ocean for a Non-Keplerian Orbit
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Callisto: a Guide to the Origin of the Jupiter System
A PAPER SUBMITTED TO THE DECADAL SURVEY ON PLANETARY SCIENCE AND ASTROBIOLOGY Callisto: A Guide to the Origin of the Jupiter System David E Smith 617-803-3377 Department of Earth, Atmospheric and PLanetary Sciences Massachusetts Institute of Technology, Cambridge MA 02139 [email protected] Co-authors: Francis Nimmo, UCSC, [email protected] Krishan Khurana, UCLA, [email protected] Catherine L. Johnson, PSI, [email protected] Mark Wieczorek, OCA, Fr, [email protected] Maria T. Zuber, MIT, [email protected] Carol Paty, University of Oregon, [email protected] Antonio Genova, Univ Rome, It, [email protected] Erwan Mazarico, NASA GSFC, [email protected] Louise Prockter, LPI, [email protected] Gregory A. Neumann, NASA GSFC Emeritus, [email protected] John E. Connerney, Adnet Systems Inc., [email protected] Edward B. Bierhaus, LMCO, [email protected] Sander J. Goossens, UMBC, [email protected] MichaeL K. Barker, NASA GSFC, [email protected] Peter B. James, Baylor, [email protected] James Head, Brown, [email protected] Jason Soderblom, MIT, [email protected] July 14, 2020 Introduction Among the GaLiLean moons of Jupiter, it is outermost CaLListo that appears to most fulLy preserve the record of its ancient past. With a surface aLmost devoid of signs of internaL geologic activity, and hints from spacecraft data that its interior has an ocean whiLe being only partiaLLy differentiated, CaLListo is the most paradoxicaL of the giant rock-ice worlds. How can a body with such a primordiaL surface harbor an ocean? If the interior was warm enough to form an ocean, how could a mixed rock and ice interior remain stable? What do the striking differences between geologicaLLy unmodified CaLListo and its sibling moon Ganymede teLL us about the formation of the GaLiLean moons and the primordiaL conditions at the time of the formation of CaLListo and the accretion of giant planet systems? The answers can be provided by a CaLListo orbitaL mission. -
The Solar System Cause Impact Craters
ASTRONOMY 161 Introduction to Solar System Astronomy Class 12 Solar System Survey Monday, February 5 Key Concepts (1) The terrestrial planets are made primarily of rock and metal. (2) The Jovian planets are made primarily of hydrogen and helium. (3) Moons (a.k.a. satellites) orbit the planets; some moons are large. (4) Asteroids, meteoroids, comets, and Kuiper Belt objects orbit the Sun. (5) Collision between objects in the Solar System cause impact craters. Family portrait of the Solar System: Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, (Eris, Ceres, Pluto): My Very Excellent Mother Just Served Us Nine (Extra Cheese Pizzas). The Solar System: List of Ingredients Ingredient Percent of total mass Sun 99.8% Jupiter 0.1% other planets 0.05% everything else 0.05% The Sun dominates the Solar System Jupiter dominates the planets Object Mass Object Mass 1) Sun 330,000 2) Jupiter 320 10) Ganymede 0.025 3) Saturn 95 11) Titan 0.023 4) Neptune 17 12) Callisto 0.018 5) Uranus 15 13) Io 0.015 6) Earth 1.0 14) Moon 0.012 7) Venus 0.82 15) Europa 0.008 8) Mars 0.11 16) Triton 0.004 9) Mercury 0.055 17) Pluto 0.002 A few words about the Sun. The Sun is a large sphere of gas (mostly H, He – hydrogen and helium). The Sun shines because it is hot (T = 5,800 K). The Sun remains hot because it is powered by fusion of hydrogen to helium (H-bomb). (1) The terrestrial planets are made primarily of rock and metal. -
Synopsis of Euler's Paper E105
1 Synopsis of Euler’s paper E105 -- Memoire sur la plus grande equation des planetes (Memoir on the Maximum value of an Equation of the Planets) Compiled by Thomas J Osler and Jasen Andrew Scaramazza Mathematics Department Rowan University Glassboro, NJ 08028 [email protected] Preface The following summary of E 105 was constructed by abbreviating the collection of Notes. Thus, there is considerable repetition in these two items. We hope that the reader can profit by reading this synopsis before tackling Euler’s paper itself. I. Planetary Motion as viewed from the earth vs the sun ` Euler discusses the fact that planets observed from the earth exhibit a very irregular motion. In general, they move from west to east along the ecliptic. At times however, the motion slows to a stop and the planet even appears to reverse direction and move from east to west. We call this retrograde motion. After some time the planet stops again and resumes its west to east journey. However, if we observe the planet from the stand point of an observer on the sun, this retrograde motion will not occur, and only a west to east path of the planet is seen. II. The aphelion and the perihelion From the sun, (point O in figure 1) the planet (point P ) is seen to move on an elliptical orbit with the sun at one focus. When the planet is farthest from the sun, we say it is at the “aphelion” (point A ), and at the perihelion when it is closest. The time for the planet to move from aphelion to perihelion and back is called the period. -
Absolute and Relative Motion Satellite Theories for Zonal and Tesseral Gravitational Harmonics
ABSOLUTE AND RELATIVE MOTION SATELLITE THEORIES FOR ZONAL AND TESSERAL GRAVITATIONAL HARMONICS A Dissertation by BHARAT MAHAJAN Submitted to the Office of Graduate and Professional Studies of Texas A&M University in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Chair of Committee, Srinivas R. Vadali Co-Chair of Committee, Kyle T. Alfriend Committee Members, John E. Hurtado Igor Zelenko Head of Department, Rodney Browersox May 2018 Major Subject: Aerospace Engineering Copyright 2018 Bharat Mahajan ABSTRACT In 1959, Dirk Brouwer pioneered the use of the Hamiltonian perturbation methods for con- structing artificial satellite theories with effects due to nonspherical gravitational perturbations in- cluded. His solution specifically accounted for the effects of the first few zonal spherical harmon- ics. However, the development of a closed-form (in the eccentricity) satellite theory that accounts for any arbitrary spherical harmonic perturbation remains a challenge to this day. In the present work, the author has obtained novel solutions for the absolute and relative motion of artificial satel- lites (absolute motion in this work refers to the motion relative to the central gravitational body) for an arbitrary zonal or tesseral spherical harmonic by using Hamiltonian perturbation methods, without resorting to expansions in either the eccentricity or the small ratio of the satellite’s mean motion and the angular velocity of the central body. First, generalized closed-form expressions for the secular, long-period, and short-period variations of the equinoctial orbital elements due to an arbitrary zonal harmonic are derived, along with the explicit expressions for the first six zonal harmonics. -
NOAA Technical Memorandum ERL ARL-94
NOAA Technical Memorandum ERL ARL-94 THE NOAA SOLAR EPHEMERIS PROGRAM Albion D. Taylor Air Resources Laboratories Silver Spring, Maryland January 1981 NOAA 'Technical Memorandum ERL ARL-94 THE NOAA SOLAR EPHEMERlS PROGRAM Albion D. Taylor Air Resources Laboratories Silver Spring, Maryland January 1981 NOTICE The Environmental Research Laboratories do not approve, recommend, or endorse any proprietary product or proprietary material mentioned in this publication. No reference shall be made to the Environmental Research Laboratories or to this publication furnished by the Environmental Research Laboratories in any advertising or sales promotion which would indicate or imply that the Environmental Research Laboratories approve, recommend, or endorse any proprietary product or proprietary material mentioned herein, or which has as its purpose an intent to cause directly or indirectly the advertised product to be used or purchased because of this Environmental Research Laboratories publication. Abstract A system of FORTRAN language computer programs is presented which have the ability to locate the sun at arbitrary times. On demand, the programs will return the distance and direction to the sun, either as seen by an observer at an arbitrary location on the Earth, or in a stan- dard astronomic coordinate system. For one century before or after the year 1960, the program is expected to have an accuracy of 30 seconds 5 of arc (2 seconds of time) in angular position, and 7 10 A.U. in distance. A non-standard algorithm is used which minimizes the number of trigonometric evaluations involved in the computations. 1 The NOAA Solar Ephemeris Program Albion D. Taylor National Oceanic and Atmospheric Administration Air Resources Laboratories Silver Spring, MD January 1981 Contents 1 Introduction 3 2 Use of the Solar Ephemeris Subroutines 3 3 Astronomical Terminology and Coordinate Systems 5 4 Computation Methods for the NOAA Solar Ephemeris 11 5 References 16 A Program Listings 17 A.1 SOLEFM . -
Architecture for Going to the Outer Solar System
ARGOSY ARGOSY: ARchitecture for Going to the Outer solar SYstem Ralph L. McNutt Jr. ll solar system objects are, in principle, targets for human in situ exploration. ARGOSY (ARchitecture for Going to the Outer solar SYstem) addresses anew the problem of human exploration to the outer planets. The ARGOSY architecture approach is scalable in size and power so that increasingly distant destinations—the systems of Jupiter, Saturn, Uranus, and Neptune—can be reached with the same crew size and time require- ments. To enable such missions, achievable technologies with appropriate margins must be used to construct a viable technical approach at the systems level. ARGOSY thus takes the step past Mars in addressing the most difficult part of the Vision for Space AExploration: To extend human presence across the solar system. INTRODUCTION The Vision for Space Exploration “The reasonable man adapts himself to the world: the unreason- 2. Extend human presence across the solar system, start- able one persists in trying to adapt the world to himself. Therefore ing with a return to the Moon by the year 2020, in 1 all progress depends on the unreasonable man.” preparation for human exploration of Mars and other G. B. Shaw destinations 3. Develop the innovative technologies, knowledge, On 14 January 2004, President Bush proposed a new and infrastructures to explore and support decisions four-point Vision for Space Exploration for NASA.2 about destinations for human exploration 1. Implement a sustained and affordable human and 4. Promote international and commercial participation robotic program to explore the solar system and in exploration to further U.S. -
Euler's Forgotten Equation of the Center
Advances in Historical Studies, 2021, 10, 44-52 https://www.scirp.org/journal/ahs ISSN Online: 2327-0446 ISSN Print: 2327-0438 Euler’s Forgotten Equation of the Center Sylvio R. Bistafa University of São Paulo, São Paulo, Brazil How to cite this paper: Bistafa, S. R. Abstract (2021). Euler’s Forgotten Equation of the Center. Advances in Historical Studies, 10, In a 1778 publication in Latin, titled Nova Methodvs Motvm Planetarvm De- 44-52. terminandi (New method to determine the motion of planets), Euler derives https://doi.org/10.4236/ahs.2021.101005 an equation of the center, which, apparently, has been forgotten. In the present work, the developments that led to Euler’s equation of the center are Received: January 9, 2021 Accepted: March 12, 2021 revisited, and applied to three planets of the Solar System. These are then Published: March 15, 2021 compared with results obtained from an equation of center that has been proposed, showing good agreement for planets with not so high eccentrici- Copyright © 2021 by author(s) and ties. Nonetheless, Euler’s derivation was not influential, and since then, the Scientific Research Publishing Inc. resulting equation of the center has been neglected by scholars and by specia- This work is licensed under the Creative Commons Attribution International lized publications alike. License (CC BY 4.0). http://creativecommons.org/licenses/by/4.0/ Keywords Open Access Euler’s Works on Astronomy, Equation of the Center, History of Orbital Calculations, Investigations on Planets’ Orbits, Astronomical Calculations, Keplerian Orbital Mechanics 1. Introduction Since antiquity, the problem of predicting the motions of the heavenly bodies has been simplified by reducing it to one of a single body in orbit about another. -
19740004369.Pdf
IA-4 TheOrbitalMechanics of Fli_htMechanics A--A Am-m ---_._ _--_-_ :5::_¸¸¸:_:::_!_:_:_i:::_!:i:_:._::::_:i_;::::,::::,:::_:.:::i::i¸:5: ::':?::!:i:!:!:!:!::':i:i:::::::;_:;::_,.'__;_:::::::........... .... ===================================================: )) T .... -...: ==================================================================================================================================== ...... :::7:_))_):)):::_:i!._...............iii_i)))))))i)i):_::_)i0j))::::!:):::))))):)).." •.........)i'::::_).............!:!:i_)i::i)iii)))))i!_. L-73-3009 Apollo 9 Landing Module as viewed from the Comm_md Module in orbit over the earth. ii ! ,\ \ i ii-il NASASP-325 TheOrbitalMechanics of Fli_htMechanics RobertScottDunnin_ LangleyResearchCenter PreparedbyNASALangleyResearchCenter Scientific and Technical ln/ormation Office 1973 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION _ Washington, D.C. If If 1 lf_;;_:'_,-li'-,,_,. A-AA A-I v_? V For sale by the National Technical Information Service Springfield, Virginia 22151 Price - Domestic, $4.75; Foreign, $7.25 Library of Congress Catalog Card Number 73-600091 ,WTT i di-ll PREFACE Despite the existence of numerous authoritative books in the field of orbital mechanics, the author has felt the need for a book which places emphasis on the con- ditions encountered with actively controlled satellites and spaceships rather than on observation and analysis of the passive heavenly bodies treated in classical astron- omy. Present-day space research, includiflg the use of computers, has made much of the material in previous books outmoded; less emphasis is now placed on closed-form solutions and more on iterative techniques. It is also apparent that a greater empha- sis on the basic formulas has become necessary. The problem of relative motion between two vehicles, which was rarely encountered in classical astronomy, has become a routine operational matter today and deserves consideration appropriate to its present importance. -
368-187 10 Q
~~ ~~ ~ ~ ~~ ~~ I . & UJJ-7- National Administration Goddard Space Flight Center Contract No. NAS-5-12487 ST - CM - 10687 ON ?HE MOTION OF REMOTE ARTIFICIAL EARTH'S SATELLITES IN 'ME GRAVITATIONAL FIELDS OF THE ENITH AND OF "€EMOON by V. P. Dolgachev * (USSR) 368-187 10 3 (ACCESSION NUMBER) 4 q P (PXGES) 'COW c 20 (CATEGORY) GPO PRICE $ io MARCH 1968 CFSTI PRICE(S) $ i .33 ' c5: Hard copy (HC) - v., Microfiche (MF) / 4,s- ff 653 July 65 1 .* . ST-(34-10687 ON 'IHE MOTION OF REMOTE ARTIFICIAL EARTH'S SATELLITES IN THE G.MVITATI0NA.L FIELDS OF THE EARTH AND OF THE MOON Vestnik Moskovskogo Universiteta by V. P. Dolgachev Astronomiya, No. 1, pp. 94 - 100, Izdatel'stvo MGU, 1968. SUMMARY The expressions are presented of first order perturbations of AES' orbit elements due to Earth's oblateness, and of the second harmonic of Moon's at- traction, the Moon being consicered as a material point moving along a circular orbit. The formulas derived are also valid for pert.urbations due to the Sun. * ** The expressions were derived in a preceding work [l] for secular varia- tions of remote AES in the gravitational fields of the Earth and of the Moon, whereupon perturbations from the second harmonic of the terrestrial potential and from the second and third harmonics of Moon's attraction were taken into account; it was moreover considered that the Moon is a material point moving along an elliptical orbit. Remaining within the framework of the classical scheme proposed by Lagran- ge, we obtained perturbations in the Lagrange elements; it is then natural that the formulas obtained for the secular perturbations are valid for small eccentricities and inclinations. -
Lecture 28: the Galilean Moons of Jupiter
Lecture 28: The Galilean Moons of Jupiter Lecture 28 The Galilean Moons of Jupiter Astronomy 141 – Winter 2012 This lecture is about the Galilean Moons of Jupiter. The Galilean moons of Jupiter are heated by tides from Jupiter – closer moons are hotter. Ganymede and Callisto are old, geologically dead worlds: mostly ice mantles over rocky cores. Innermost Io is tidally melted inside, making it the most volcanically active world in the Solar System. Europa may have liquid water oceans beneath the ice, making it the most promising place to search for life. The Galilean Moons of Jupiter Io Europa Ganymede Callisto (3642 km) (3130 km) (5262 km) (4806 km) Moon (3474 km) Astronomy 141 - Winter 2012 1 Lecture 28: The Galilean Moons of Jupiter The Galilean Moons all orbit in the same direction around Jupiter. The inner 3 are on resonant orbits. Orbital Periods: Io: 1.8 days Europa Europa: 3.6 days Ganymede (2 times Io's period) Ganymede: 7.2 days Callisto (4 times Io's period) Io Callisto: 16.7 days Innermost are strongly affected by tides from Jupiter Liquid H2O @ 1atm Cold Interior Ganymede & Callisto are mixed ice & rock, low- density moons. Mean densities of 1.9 & 1.8 g/cc, respectively Deep ice mantles over rocky/icy cores. Ganymede Old, heavily cratered surfaces They lack internal heat and Callisto are geologically inactive. Astronomy 141 - Winter 2012 2 Lecture 28: The Galilean Moons of Jupiter In the terrestrial planets, interior heat is determined by the planet’s size. Large Earth & Venus have hot interiors: Smaller Mercury, Moon & Mars have cold interiors. -
Equation of Time - Wikipedia
12/2/2018 Equation of time - Wikipedia Equation of time The equation of time describes the discrepancy between two kinds of solar time. The word equation is used in the medieval sense of "reconcile a difference". The two times that differ are the apparent solar time, which directly tracks the diurnal motion of the Sun, and mean solar time, which tracks a theoretical mean Sun with noons 24 hours apart. Apparent solar time can be obtained by measurement of the current position (hour angle) of the Sun, as indicated (with limited accuracy) by a sundial. Mean solar time, for the same place, would be the time indicated by a steady clock set so that over the year its differences from apparent solar time would resolve to zero.[1] The equation of time is the east or west component of the analemma, a curve representing the angular offset of the Sun from its mean position on the celestial sphere as viewed from Earth. The equation of time values for each day of the year, compiled by astronomical observatories, were widely listed in almanacs and ephemerides.[2][3] The equation of time — above the axis a sundial will appear fast relative to a clock showing local mean Contents time, and below the axis a sundial will appear slow. The concept Sign of the equation of time History Ancient history — Babylon and Egypt Medieval and Renaissance astronomy Apparent time versus mean time 18th and early 19th centuries Major components of the equation Eccentricity of the Earth's orbit Obliquity of the ecliptic Secular effects Graphical representation https://en.wikipedia.org/wiki/Equation_of_time 1/20 12/2/2018 Equation of time - Wikipedia Practical use Calculating the equation of time Mathematical description Right ascension calculation Equation of time Remark on the continuity of the equation of time Secular effects Alternative calculation Addendum about solar declination See also Notes and Footnotes This graph uses the opposite sign to the one above References it. -
A Mean Elements Orbit Propagator Program for Highly Elliptical Orbits
CEAS Space Journal manuscript No. (will be inserted by the editor) HEOSAT: A mean elements orbit propagator program for Highly Elliptical Orbits Martin Lara · Juan F. San-Juan · Denis Hautesserres CEAS Space Journal (ISSN: 1868-2502, ESSN: 1868-2510) (2018) doi:10.1007/s12567-017-0152-x (Pre-print version) Abstract The algorithms used in the construction of a semi- intermediary solutions to the J2 problem [34,11], the contin- analytical propagator for the long-term propagation of High- uous increase in the accuracy of observations demanded the ly Elliptical Orbits (HEO) are described. The software prop- use of more complex dynamical models to achieve a sim- agates mean elements and include the main gravitational and ilar precision in the orbit predictions. In particular higher non-gravitational effects that may affect common HEO or- degrees in the Legendre polynomials expansion of the third- bits, as, for instance, geostationary transfer orbits or Mol- body disturbing function are commonly required (see [17, niya orbits. Comparisons with numerical integration show 24], for instance). Useful analytical theories needed to deal that it provides good results even in extreme orbital config- with a growing number of effects, a fact that made that the urations, as the case of SymbolX. trigonometric series evaluated by the theory comprised tens of thousands of terms [5]. Keywords HEO · Geopotential · third-body perturbation · In an epoch of computational plenty, the vast possibili- tesseral resonances · SRP · atmospheric drag · mean ties offered by special perturbation methods clearly surpass elements · semi-analytic propagation those of general perturbation methods in their traditional application to orbit propagation.