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Cornell University Ithaca, New York 14650 JOSE - JUPITER ORBITING SPACECRAFT
N T Z 33854 C *?** IS81 1? JOSE - JUPITER ORBITING SPACECRAFT: A SYSTEMS STUDY Volume I '>•*,' T COLLEGE OF ENGINEERING Cornell University Ithaca, New York 14650 JOSE - JUPITER ORBITING SPACECRAFT: A SYSTEMS STUDY Volume I Prepared Under Contract No. NGR 33-010-071 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION by NASA-Cornell Doctoral Design Trainee Group (196T-TO) October 1971 College of Engineering Cornell University Ithaca, New York Table of Contents Volume I Preface Chapter I: The Planet Jupiter: A Brief Summary B 1-2 r. Mechanical Properties of the Planet Jupiter. P . T-fi r> 1-10 F T-lfi F T-lfi 0 1-29 H, 1-32 T 1-39 References ... p. I-k2 Chapter II: The Spacecraft Design and Mission Definition A. Introduction p. II-l B. Organizational Structure and the JOSE Mission p. II-l C. JOSE Components p. II-1* D. Proposed Configuration p. II-5 Bibliography and References p. 11-10 Chapter III: Mission Trajectories A. Interplanetary Trajectory Analysis .... p. III-l B. Jupiter Orbital Considerations p. III-6 Bibliography and References. p. 111-38 Chapter IV: Attitude Control A. Introduction and Summary . p. IV-1 B. Expected Disturbance Moments M in Interplanetary Space . p. IV-3 C. Radiation-Produced Impulse Results p. IV-12 D. Meteoroid-Produced Impulse Results p. IV-13 E. Inertia Wheel Analysis p. IV-15 F. Attitude System Tradeoff Analysis p. IV-19 G. Conclusion P. IV-21 References and Bibliography p. TV-26 Chapter V: Propulsion Subsystem A. Mission Requirements p. V-l B. Orbit Insertion Analysis p. -
Arxiv:1303.4129V2 [Gr-Qc] 8 May 2013 Counters with Supermassive Black Holes (SMBH) of Mass in Some Preceding Tidal Event
Relativistic effects in the tidal interaction between a white dwarf and a massive black hole in Fermi normal coordinates Roseanne M. Cheng∗ Center for Relativistic Astrophysics, School of Physics, Georgia Institute of Technology, Atlanta, Georgia 30332, USA and Department of Physics and Astronomy, University of North Carolina, Chapel Hill, North Carolina 27599, USA Charles R. Evansy Department of Physics and Astronomy, University of North Carolina, Chapel Hill, North Carolina 27599 (Received 17 March 2013; published 6 May 2013) We consider tidal encounters between a white dwarf and an intermediate mass black hole. Both weak encounters and those at the threshold of disruption are modeled. The numerical code combines mesh-based hydrodynamics, a spectral method solution of the self-gravity, and a general relativistic Fermi normal coordinate system that follows the star and debris. Fermi normal coordinates provide an expansion of the black hole tidal field that includes quadrupole and higher multipole moments and relativistic corrections. We compute the mass loss from the white dwarf that occurs in weak tidal encounters. Secondly, we compute carefully the energy deposition onto the star, examining the effects of nonradial and radial mode excitation, surface layer heating, mass loss, and relativistic orbital motion. We find evidence of a slight relativistic suppression in tidal energy transfer. Tidal energy deposition is compared to orbital energy loss due to gravitational bremsstrahlung and the combined losses are used to estimate tidal capture orbits. Heating and partial mass stripping will lead to an expansion of the white dwarf, making it easier for the star to be tidally disrupted on the next passage. -
Astrometry and Tidal Migration V
Astrometry and tidal migration V. Lainey (JPL/IMCCE), J.Fuller (Caltech) [email protected] -KISS workshop- October 16th 2018 Astrometric measurements Example 1: classical astrometric observations (the most direct measurement) Images suitable for astrometric reduction from ground or space Tajeddine et al. 2013 Mallama et al. 2004 CCD obs from ground Cassini ISS image HST image Photographic plates (not used anymore BUT re-reduction now benefits from modern scanning machine) Astrometric measurements Example 2: photometric measurements (undirect astrometric measurement) Eclipses by the planet Mutual phenomenae (barely used those days…) (arising every six years) By modeling the event, one can solve for mid-time event and minimum distance between the center of flux figure of the objects à astrometric measure Time (hours) Astrometric measurements Example 3: other measurements (non exhaustive list) During flybys of moons, one can (sometimes!) solved for a correction on the moon ephemeris Radio science measurement (orbital tracking) Radar measurement (distance measurement between back and forth radio wave travel) Morgado et al. 2016 Mutual approximation (measure of moons’ distance rate) Astrometric accuracy Remark: 1- Accuracy of specific techniques STRONGLY depends on the epoch 2- Total numBer of oBservations per oBservation opportunity can Be VERY different For the Galilean system: (numbers are purely indicative) From ground Direct imaging: 100 mas (300 km) to 20 mas (60 km) –stacking techniques- Mutual events: typically 20-80 mas -
Effect of Mantle and Ocean Tides on the Earth’S Rotation Rate
A&A 493, 325–330 (2009) Astronomy DOI: 10.1051/0004-6361:200810343 & c ESO 2008 Astrophysics Effect of mantle and ocean tides on the Earth’s rotation rate P. M. Mathews1 andS.B.Lambert2 1 Department of Theoretical Physics, University of Madras, Chennai 600025, India 2 Observatoire de Paris, Département Systèmes de Référence Temps Espace (SYRTE), CNRS/UMR8630, 75014 Paris, France e-mail: [email protected] Received 7 June 2008 / Accepted 17 October 2008 ABSTRACT Aims. We aim to compute the rate of increase of the length of day (LOD) due to the axial component of the torque produced by the tide generating potential acting on the tidal redistribution of matter in the oceans and the solid Earth. Methods. We use an extension of the formalism applied to precession-nutation in a previous work to the problem of length of day variations of an inelastic Earth with a fluid core and oceans. Expressions for the second order axial torque produced by the tesseral and sectorial tide-generating potentials on the tidal increments to the Earth’s inertia tensor are derived and used in the axial component of the Euler-Liouville equations to arrive at the rate of increase of the LOD. Results. The increase in the LOD, produced by the same dissipative mechanisms as in the theoretical work on which the IAU 2000 nutation model is based and in our recent computation of second order effects, is found to be at a rate of 2.35 ms/cy due to the ocean tides, and 0.15 ms/cy due to solid Earth tides, in reasonable agreement with estimates made by other methods. -
Adaptive Multibody Gravity Assist Tours Design in Jovian System for the Ganymede Landing
TO THE ADAPTIVE MULTIBODY GRAVITY ASSIST TOURS DESIGN IN JOVIAN SYSTEM FOR THE GANYMEDE LANDING Grushevskii A.V.(1), Golubev Yu.F.(2), Koryanov V.V.(3), and Tuchin A.G.(4) (1)KIAM (Keldysh Institute of Applied Mathematics), Miusskaya sq., 4, Moscow, 125047, Russia, +7 495 333 8067, E-mail: [email protected] (2)KIAM, Miusskaya sq., 4, Moscow, 125047, Russia, E-mail: [email protected] (3)KIAM, Miusskaya sq., 4, Moscow, 125047, Russia, E-mail: [email protected] (4)KIAM, Miusskaya sq., 4, Moscow, 125047, Russia, E-mail: [email protected] Keywords: gravity assist, adaptive mission design, trajectory design, TID, phase beam Introduction Modern space missions inside Jovian system are not possible without multiple gravity assists (as well as in Saturnian system, etc.). The orbit design for real upcoming very complicated missions by NASA, ESA, RSA should be adaptive to mission parameters, such as: the time of Jovian system arrival, incomplete information about ephemeris of Galilean Moons and their gravitational fields, errors of flybys implementation, instrumentation deflections. Limited dynamic capabilities, taking place in case of maneuvering around Jupiter's moons, demand multiple encounters (about 15-30 times) for these purposes. Flexible algorithm of current mission scenarios synthesis (specially selected) and their operative transformation is required. Mission design is complicated due to requirements of the Ganymede Orbit Insertion (GOI) ("JUICE" ESA) and also Ganymede Landing implementation ("Laplas-P" RSA [1]) comparing to the ordinary early ―velocity gain" missions since ―Pioneers‖ and "Voyagers‖. Thus such scenario splits in two parts. Part 1(P1), as usually, would be used to reduce the spacecraft’s orbital energy with respect to Jupiter and set up the conditions for more frequent flybys. -
Our Planetary System (Chapter 7) Based on Chapter 7
Our Planetary System (Chapter 7) Based on Chapter 7 • This material will be useful for understanding Chapters 8, 9, 10, 11, and 12 on “Formation of the solar system”, “Planetary geology”, “Planetary atmospheres”, “Jovian planet systems”, and “Remnants of ice and rock” • Chapters 3 and 6 on “The orbits of the planets” and “Telescopes” will be useful for understanding this chapter Goals for Learning • How do planets rotate on their axes and orbit the Sun? • What are the planets made of? • What other classes of objects are there in the solar system? Orbits mostly lie in the same flat plane All planets go around the Sun in the same direction Most orbits are close to circular Not coincidences! Most planets rotate in the same “sense” as they orbit the Sun Coincidence? Planetary equators mostly lie in the same plane as their orbits Coincidence? • Interactive Figure: Orbital and Rotational Properties of the Planets Rotation and Orbits of Moons • Most moons (especially the larger ones) orbit in near-circular orbits in the same plane as the equator of their parent planet • Most moons rotate so that their equator is in the plane of their orbit • Most moons rotate in the same “sense” as their orbit around the parent planet • Everything is rotating/orbiting in the same direction A Brief Tour • Distance from Sun •Size •Mass • Composition • Temperature • Rings/Moons Sun 695000 km = 108 RE 333000 MEarth 98% Hydrogen and helium 99.9% total mass of solar system Surface = 5800K Much hotter inside Giant ball of gas Gravity => orbits Heat/light => weather -
Jupiter Mass
CESAR Science Case Jupiter Mass Calculating a planet’s mass from the motion of its moons Student’s Guide Mass of Jupiter 2 CESAR Science Case Table of Contents The Mass of Jupiter ........................................................................... ¡Error! Marcador no definido. Kepler’s Three Laws ...................................................................................................................................... 4 Activity 1: Properties of the Galilean Moons ................................................................................................. 6 Activity 2: Calculate the period of your favourite moon ................................................................................. 9 Activity 3: Calculate the orbital radius of your favourite moon .................................................................... 12 Activity 4: Calculate the Mass of Jupiter ..................................................................................................... 15 Additional Activity: Predict a Transit ............................................................................................................ 16 To know more… .......................................................................................................................... 19 Links ............................................................................................................................................ 19 Mass of Jupiter 3 CESAR Science Case Background Kepler’s Three Laws The three Kepler’s Laws, published between -
The Effect of Jupiter\'S Mass Growth on Satellite Capture
A&A 414, 727–734 (2004) Astronomy DOI: 10.1051/0004-6361:20031645 & c ESO 2004 Astrophysics The effect of Jupiter’s mass growth on satellite capture Retrograde case E. Vieira Neto1;?,O.C.Winter1, and T. Yokoyama2 1 Grupo de Dinˆamica Orbital & Planetologia, UNESP, CP 205 CEP 12.516-410 Guaratinguet´a, SP, Brazil e-mail: [email protected] 2 Universidade Estadual Paulista, IGCE, DEMAC, CP 178 CEP 13.500-970 Rio Claro, SP, Brazil e-mail: [email protected] Received 13 June 2003 / Accepted 12 September 2003 Abstract. Gravitational capture can be used to explain the existence of the irregular satellites of giants planets. However, it is only the first step since the gravitational capture is temporary. Therefore, some kind of non-conservative effect is necessary to to turn the temporary capture into a permanent one. In the present work we study the effects of Jupiter mass growth for the permanent capture of retrograde satellites. An analysis of the zero velocity curves at the Lagrangian point L1 indicates that mass accretion provides an increase of the confinement region (delimited by the zero velocity curve, where particles cannot escape from the planet) favoring permanent captures. Adopting the restricted three-body problem, Sun-Jupiter-Particle, we performed numerical simulations backward in time considering the decrease of M . We considered initial conditions of the particles to be retrograde, at pericenter, in the region 100 R a 400 R and 0 e 0:5. The results give Jupiter’s mass at the X moment when the particle escapes from the planet. -
A Possible Explanation of the Secular Increase of the Astronomical Unit 1
T. Miura 1 A possible explanation of the secular increase of the astronomical unit Takaho Miura(a), Hideki Arakida, (b) Masumi Kasai(a) and Syuichi Kuramata(a) (a)Faculty of Science and Technology,Hirosaki University, 3 bunkyo-cyo Hirosaki, Aomori, 036-8561, Japan (b)Education and integrate science academy, Waseda University,1 waseda sinjuku Tokyo, Japan Abstract We give an idea and the order-of-magnitude estimations to explain the recently re- ported secular increase of the Astronomical Unit (AU) by Krasinsky and Brumberg (2004). The idea proposed is analogous to the tidal acceleration in the Earth-Moon system, which is based on the conservation of the total angular momentum and we apply this scenario to the Sun-planets system. Assuming the existence of some tidal interactions that transfer the rotational angular momentum of the Sun and using re- d ported value of the positive secular trend in the astronomical unit, dt 15 4(m/s),the suggested change in the period of rotation of the Sun is about 21(ms/cy) in the case that the orbits of the eight planets have the same "expansionrate."This value is suf- ficiently small, and at present it seems there are no observational data which exclude this possibility. Effects of the change in the Sun's moment of inertia is also investi- gated. It is pointed out that the change in the moment of inertia due to the radiative mass loss by the Sun may be responsible for the secular increase of AU, if the orbital "expansion"is happening only in the inner planets system. -
Tidal Locking and the Gravitational Fold Catastrophe
City University of New York (CUNY) CUNY Academic Works Publications and Research New York City College of Technology 2020 Tidal locking and the gravitational fold catastrophe Andrea Ferroglia CUNY New York City College of Technology Miguel C. N. Fiolhais CUNY Borough of Manhattan Community College How does access to this work benefit ou?y Let us know! More information about this work at: https://academicworks.cuny.edu/ny_pubs/679 Discover additional works at: https://academicworks.cuny.edu This work is made publicly available by the City University of New York (CUNY). Contact: [email protected] Tidal locking and the gravitational fold catastrophe Andrea Ferroglia1;2 and Miguel C. N. Fiolhais3;4 1The Graduate School and University Center, The City University of New York, 365 Fifth Avenue, New York, NY 10016, USA 2 Physics Department, New York City College of Technology, The City University of New York, 300 Jay Street, Brooklyn, NY 11201, USA 3 Science Department, Borough of Manhattan Community College, The City University of New York, 199 Chambers St, New York, NY 10007, USA 4 LIP, Departamento de F´ısica, Universidade de Coimbra, 3004-516 Coimbra, Portugal The purpose of this work is to study the phenomenon of tidal locking in a pedagogical framework by analyzing the effective gravitational potential of a two-body system with two spinning objects. It is shown that the effective potential of such a system is an example of a fold catastrophe. In fact, the existence of a local minimum and saddle point, corresponding to tidally-locked circular orbits, is regulated by a single dimensionless control parameter which depends on the properties of the two bodies and on the total angular momentum of the system. -
Tidal Tomography to Probe the Moon's Mantle Structure Using
Tidal Tomography to Probe the Moon’s Mantle Structure Using Lunar Surface Gravimetry Kieran A. Carroll1, Harriet Lau2, 1: Gedex Systems Inc., [email protected] 2: Department of Earth and Planetary Sciences, Harvard University, [email protected] Lunar Tides Gravimetry of the Lunar Interior VEGA Instrument through the Moon's PulSE • Gedex has developed a low cost compact space gravimeter instrument , VEGA (Vector (GLIMPSE) Investigation Gravimeter/Accelerometer) Moon • Currently this is the only available gravimeter that is suitable for use in space Earth GLIMPSE Investigation: • Proposed under NASA’s Lunar Surface Instrument and Technology Payloads • ca. 1972 MIT developed a space gravimeter (LSITP) program. instrument for use on the Moon, for Apollo 17. That instrument is long-ago out of • To fly a VEGA instrument to the Moon on a commercial lunar lander, via NASA’s production and obsolete. Commercial Lunar Payload Services (CLPS) program. VEGA under test in thermal- GLIMPSE Objectives: VEGA Space Gravimeter Information vacuum chamber at Gedex • Prove the principle of measuring time-varying lunar surface gravity to probe the lunar • Measures absolute gravity vector, with no • Just as the Moon and the Sun exert tidal forces on the Earth, the Earth exerts tidal deep interior using the Tidal Tomography technique. bias forces on the Moon. • Determine constraints on parameters defining the Lunar mantle structure using time- • Accuracy on the Moon: • Tidal stresses in the Moon are proportional to the gravity gradient tensor field at the varying gravity measurements at a location on the surface of the Moon, over the • Magnitude: Effective noise of 8 micro- Moon’s centre, multiplies by the distance from the Moon’s centre. -
Cold Plasma Diagnostics in the Jovian System
341 COLD PLASMA DIAGNOSTICS IN THE JOVIAN SYSTEM: BRIEF SCIENTIFIC CASE AND INSTRUMENTATION OVERVIEW J.-E. Wahlund(1), L. G. Blomberg(2), M. Morooka(1), M. André(1), A.I. Eriksson(1), J.A. Cumnock(2,3), G.T. Marklund(2), P.-A. Lindqvist(2) (1)Swedish Institute of Space Physics, SE-751 21 Uppsala, Sweden, E-mail: [email protected], [email protected], mats.andré@irfu.se, [email protected] (2)Alfvén Laboratory, Royal Institute of Technology, SE-100 44 Stockholm, Sweden, E-mail: [email protected], [email protected], [email protected], per- [email protected] (3)also at Center for Space Sciences, University of Texas at Dallas, U.S.A. ABSTRACT times for their atmospheres are of the order of a few The Jovian magnetosphere equatorial region is filled days at most. These atmospheres can therefore rightly with cold dense plasma that in a broad sense co-rotate with its magnetic field. The volcanic moon Io, which be termed exospheres, and their corresponding ionized expels sodium, sulphur and oxygen containing species, parts can be termed exo-ionospheres. dominates as a source for this cold plasma. The three Observations indicate that the exospheres of the three icy Galilean moons (Callisto, Ganymede, and Europa) icy Galilean moons (Europa, Ganymede and Callisto) also contribute with water group and oxygen ions. are oxygen rich [1, 2]. Several authors have also All the Galilean moons have thin atmospheres with modelled these exospheres [3, 4, 5], and the oxygen was residence times of a few days at most.