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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 -
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur To cite this version: Alex Soumbatov-Gur. Phobos, Deimos: Formation and Evolution. [Research Report] Karpov institute of physical chemistry. 2019. hal-02147461 HAL Id: hal-02147461 https://hal.archives-ouvertes.fr/hal-02147461 Submitted on 4 Jun 2019 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur The moons are confirmed to be ejected parts of Mars’ crust. After explosive throwing out as cone-like rocks they plastically evolved with density decays and materials transformations. Their expansion evolutions were accompanied by global ruptures and small scale rock ejections with concurrent crater formations. The scenario reconciles orbital and physical parameters of the moons. It coherently explains dozens of their properties including spectra, appearances, size differences, crater locations, fracture symmetries, orbits, evolution trends, geologic activity, Phobos’ grooves, mechanism of their origin, etc. The ejective approach is also discussed in the context of observational data on near-Earth asteroids, main belt asteroids Steins, Vesta, and Mars. The approach incorporates known fission mechanism of formation of miniature asteroids, logically accounts for its outliers, and naturally explains formations of small celestial bodies of various sizes. -
Mars, Phobos, and Deimos Sample Return Enabled by ARRM Alternative Trade Study Spacecraft
Mars, Phobos, and Deimos Sample Return Enabled by ARRM Alternative Trade Study Spacecraft Jacob A. Englander,∗ Matthew A. Vavrina,† Bo Naasz ,‡ Raymond G. Merill,MinQu§ ¶ The Asteroid Robotic Redirect Mission (ARRM) has been the topic of many mission design studies since 2011.1 The reference ARRM spacecraft uses a powerful solar electric propulsion (SEP) system and a bag device to capture a small asteroid from an Earth-like orbit and redirect it to a distant retrograde orbit (DRO) around the moon. The ARRM Option B spacecraft uses the same propulsion system and multi-Degree of Freedom (DoF) manipulators device to retrieve a very large sample (thousands of kilograms) from a 100+ meter diameter farther-away Near Earth Asteroid (NEA). This study will demonstrate that the ARRM Option B spacecraft design can also be used to return samples from Mars and its moons - either by acquiring a large rock from the surface of Phobos or Deimos, and/or by rendezvousing with a sample-return spacecraft launched from the surface of Mars. I. Introduction The Asteroid Robotic Redirect Mission (ARRM) Option A concept, first introduced in 2011,1 is a mission design to capture and return a small near-Earth asteroid (NEA) to cislunar space. The ARRM Option B concept is a similar spacecraft, but designed to return a very large sample from a more difficult to reach NEA.2 In this work we show that the spacecraft designed for ARRM Option B is also well-suited to sample return from Mars and its moons. This work presents low-thrust interplanetary trajectories from cislunar space to Mars and back, including descent from the Martian sphere of influence (SOI) to the desired orbit altitude and ascent to the SOI after the sample retrieval is complete. -
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. -
Deimos and Phobos As Destinations for Human Exploration
Deimos and Phobos as Destinations for Human Exploration Josh Hopkins Space Exploration Architect Lockheed Martin Caltech Space Challenge March 2013 © 2013 Lockheed Martin Corporation. All Rights Reserved 1 Topics • Related Lockheed Martin mission studies • Orbital mechanics vs solar cycles • Relevant characteristics of Phobos and Deimos • Locations to land • Considerations for designing your mission • Suggested trades 2 Stepping Stones Stepping Stones is a series of exploration 2023 missions building incrementally towards Deimos Scout the long term goal of exploring Mars. Each mission addresses science objectives relating to the formation of the solar 2031-2035 system and the origins of life. Red Rocks: explore Mars from Deimos 2024, 2025, 2029 2017 Plymouth Rock: Humans explore asteroids like Asteroid scout 1999 AO10 and 2000 SG344 2018-2023 Fastnet: Explore the Moon’s far side from Earth-Moon L2 region 2016 Asteroid survey 2017 SLS test flight 2013-2020 Human systems tests on ISS Lockheed Martin Notional Concept Dates subject to change 3 Deimos photo courtesy of NASA-JPL, University of Arizona Summary • A human mission to one of the two moons of Mars would be an easier precursor to a mission to land on Mars itself. • Astronauts would explore the moon in person and teleoperate rovers on the surface of Mars with minimal lag time, with the goal of returning samples to Earth. • “Red Rocks” mission to land on a Martian moon would follow “Plymouth Rock” missions to a Near Earth Asteroid. • Comparison of Deimos and Phobos revealed Deimos is the preferred destination for this mission. • We identified specific areas on Deimos and Phobos as optimal landing sites for an early mission focused on teleoperation. -
The Moon (~1700Km) an Asteroid (~50Km)
1) inventory Solar System 2) spin/orbit/shape 3) heated by the Sun overview 4) how do we fnd out Inventory 1 star (99.9% of M) 8 planets (99.9% of L) - Terrestrial: Mercury Venus Earth Mars - Giant: Jupiter Saturn Uranus Neptune Lots of small bodies incl. dwarf planets Ceres Pluto Eris Maybe a 9th planet? Moons of Jupiter Inventory (cont'd) 4 Galilean satellites (Ganymede, Callisto, Io & Europa), 3 Many moons & rings ~10 km (close to Jupiter, likely primordial) Mercury: 0 Venus: 0 Earth: 1 (1700km) Mars: 2 (~10km) Jupiter: 69 + rings Saturn: 62 + rings Uranus: 27 + rings Neptune: 14 + rings 2001J3: 4km Even among dwarf planets, asteroids, Kuiper belt objects, and comets. E.g., Pluto: 5 Eris: 1 Moons of Mars: Deimos & Phobos, ~10km Atmosphere no thick thick little thick Inventory (cont'd) ~105 known small objects in the - Asteroid belt (Ceres ~300 km) - Kuiper belt (Eris, Pluto, Sedna, Quaoar, ~1000 km) Estimated: ~1012 comets in the - Oort cloud (~ 104 AU) Associated: - zodiacal dust (fre-works on the sky: comets & meteorites) What are planets? IAU (for solar system): Orbits Sun, massive enough to be round and to have cleared its neighbourhood. More general: 6 1) no nuclear fusion (not even deuterium): Tc < 10 K 2) pressure provided by electron degeneracy and/or Coulomb force (l ~ h/p ~ d) (d ~ atomic radius) 3) can be solid or gaseous (with solid cores) --- similar density Mass & Mean r M [g/cm3] R~M J Jupiter 1.0 1.33 R R~M1/3 Saturn 0.3 0.77 R~M-1/3 Neptune 0.05 1.67 Uranus 0.04 1.24 Earth 0.003 5.52 Venus 0.002 5.25 planets brown dwarfs stars Mars 0.0003 3.93 Mercury 0.0002 5.43 3 MJ 13 MJ 80 MJ M Orbits inclination: largely coplanar (history) direction: all the same eccentricity: a few percent (except for Mercury) Titus-Bode (ftting) law (1766) planetary orbits appear to (almost) satisfy a single relation 'Predict' the existence of the asteroid belt (1801: Ceres discovered) coincidence or something deeper? other systems? Computer simulations indicate that planets are as maximally packed as allowed by stability. -