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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. -
Planet Formation
3. Planet form ation Frontiers of A stronom y W orkshop/S chool Bibliotheca A lexandrina M arch-A pril 2006 Properties of planetary system s • all giant planets in the solar system have a > 5 A U w hile extrasolar giant planets have semi-major axes as small as a = 0.02 A U • planetary orbital angular momentum is close to direction of S un’s spin angular momentum (w ithin 7o) • 3 of 4 terrestrial planets and 3 of 4 giant planets have obliquities (angle betw een spin and orbital angular momentum) < 30o • interplanetary space is virtually empty, except for the asteroid belt and the Kuiper belt • planets account for < 0.2% of mass of solar system but > 98% of angular momentum Properties of planetary system s • orbits of major planets in solar system are nearly circular (eMercury=0.206, ePluto=0.250); orbits of extrasolar planets are not (emedian=0.28) • probability of finding a planet is proportional to mass of metals in the star Properties of planetary system s • planets suffer no close encounters and are spaced fairly n regularly (Bode’s law : an=0.4 + 0.3×2 ) planet semimajor axis (A U ) n an (A U ) Mercury 0.39 −∞ 0.4 V enus 0.72 0 0.7 Earth 1.00 1 1.0 Mars 1.52 2 1.6 asteroids 2.77 (Ceres) 3 2.8 Jupiter 5.20 4 5.2 S aturn 9.56 5 10.0 U ranus 19.29 6 19.6 N eptune 30.27 7 38.8 Pluto 39.68 8 77.2 Properties of planetary system s • planets suffer no close encounters and are spaced fairly n regularly (Bode’s law : an=0.4 + 0.3×2 ) planet semimajor axis (A U ) n an (A U ) Mercury+ 0.39 −∞ 0.4 V enus 0.72 0 0.7 Earth 1.00 1 1.0 *predicted -
Planets of the Solar System
Chapter Planets of the 27 Solar System Chapter OutlineOutline 1 ● Formation of the Solar System The Nebular Hypothesis Formation of the Planets Formation of Solid Earth Formation of Earth’s Atmosphere Formation of Earth’s Oceans 2 ● Models of the Solar System Early Models Kepler’s Laws Newton’s Explanation of Kepler’s Laws 3 ● The Inner Planets Mercury Venus Earth Mars 4 ● The Outer Planets Gas Giants Jupiter Saturn Uranus Neptune Objects Beyond Neptune Why It Matters Exoplanets UnderstandingU d t di theth formationf ti and the characteristics of our solar system and its planets can help scientists plan missions to study planets and solar systems around other stars in the universe. 746 Chapter 27 hhq10sena_psscho.inddq10sena_psscho.indd 774646 PDF 88/15/08/15/08 88:43:46:43:46 AAMM Inquiry Lab Planetary Distances 20 min Turn to Appendix E and find the table entitled Question to Get You Started “Solar System Data.” Use the data from the How would the distance of a planet from the sun “semimajor axis” row of planetary distances to affect the time it takes for the planet to complete devise an appropriate scale to model the distances one orbit? between planets. Then find an indoor or outdoor space that will accommodate the farthest distance. Mark some index cards with the name of each planet, use a measuring tape to measure the distances according to your scale, and place each index card at its correct location. 747 hhq10sena_psscho.inddq10sena_psscho.indd 774747 22/26/09/26/09 111:42:301:42:30 AAMM These reading tools will help you learn the material in this chapter. -
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. -
Meteorites and the Origin of the Solar System
Meteorites and the origin of the solar system STEPHEN G. BRUSH University of Maryland, College Park, MD 20742, USA (e-mail: [email protected]) Abstract: During the past two centuries, theories of the origin of the solar system have been strongly influenced by observations and theories about meteorites. I review this history up to about 1985. During the 19th century the hypothesis that planets formed by accretion of small solid particles ('the meteoritic hypothesis') competed with the alternative 'nebular hypothesis' of Laplace, based on condensation from a hot gas. At the beginning of the 20th century Chamberlin and Moulton revived the meteoritic hypothesis as the 'planetesimal hypothesis' and joined it to the assumption that the solar system evolved from the encounter of the Sun with a passing star. Later, the encounter hypothesis was rejected and the planetesimal hypothesis was incorporated into new versions of the nebular hypothesis. In the 1950s, meteorites provided essential data for the establishment by Patterson and others of the pre- sently accepted 4500 Ma age of the Earth and the solar system. Analysis of the Allende meteorite, which fell in 1969, inspired the 'supernova trigger' theory of the origin of the solar system, and furnished useful constraints on theories of planetary formation developed by Urey, Ringwood, Anders and others. Many of these theories assumed condensation from a homogeneous hot gas, an assumption that was challenged by astrophysical calculations. The meteoritic-planetesimal theory of planet formation was developed in Russia by Schmidt and later by Safronov. Wetherill, in the United States, established it as the preferred theory for formation of terrestrial planets. -
PHYS133 – Lab 4 the Revolution of the Moons of Jupiter
PHYS133 – Lab 4 The Revolution of the Moons of Jupiter Goals: Use a simulated remotely controlled telescope to observe Jupiter and the position of its four largest moons. Plot their positions relative to the planet vs. time and fit a curve to them to determine their orbit characteristics (i.e., period and semi‐major axis). Employ Newton’s form of Kepler’s third law to determine the mass of Jupiter. What You Turn In: Graphs of your orbital data for each moon. Calculations of the mass of Jupiter for each moon’s orbit. Calculate the time required to go to Mars from Earth using the lowest possible energy. Background Reading: Background reading for this lab can be found in your text book (specifically, Chapters 3 and 4 and especially section 4.4) and the notes for the course. Equipment provided by the lab: Computer with Internet Connection • Project CLEA program “The Revolutions of the Moons of Jupiter” Equipment provided by the student: Pen Calculator Background: Astronomers cannot directly measure many of the things they study, such as the masses and distances of the planets and their moons. Nevertheless, we can deduce some properties of celestial bodies from their motions despite the fact that we cannot directly measure them. In 1543, Nicolaus Copernicus hypothesized that the planets revolve in circular orbits around the sun. Tycho Brahe (1546‐1601) carefully observed the locations of the planets and 777 stars over a period of 20 years using a sextant and compass. These observations were used by Johannes Kepler, to deduce three empirical mathematical laws governing the orbit of one object around another. -
Arxiv:1209.5996V1 [Astro-Ph.EP] 26 Sep 2012 1.1
, 1{28 Is the Solar System stable ? Jacques Laskar ASD, IMCCE-CNRS UMR8028, Observatoire de Paris, UPMC, 77 avenue Denfert-Rochereau, 75014 Paris, France [email protected] R´esum´e. Since the formulation of the problem by Newton, and during three centuries, astrono- mers and mathematicians have sought to demonstrate the stability of the Solar System. Thanks to the numerical experiments of the last two decades, we know now that the motion of the pla- nets in the Solar System is chaotic, which prohibits any accurate prediction of their trajectories beyond a few tens of millions of years. The recent simulations even show that planetary colli- sions or ejections are possible on a period of less than 5 billion years, before the end of the life of the Sun. 1. Historical introduction 1 Despite the fundamental results of Henri Poincar´eabout the non-integrability of the three-body problem in the late 19th century, the discovery of the non-regularity of the Solar System's motion is very recent. It indeed required the possibility of calculating the trajectories of the planets with a realistic model of the Solar System over very long periods of time, corresponding to the age of the Solar System. This was only made possible in the past few years. Until then, and this for three centuries, the efforts of astronomers and mathematicians were devoted to demonstrate the stability of the Solar System. arXiv:1209.5996v1 [astro-ph.EP] 26 Sep 2012 1.1. Solar System stability The problem of the Solar System stability dates back to Newton's statement concerning the law of gravitation. -
Allowed Planetary Orbits
RELATIONSHIPS OF PARAMETERS OF PLANETARY ORBITS IN SOLAR---TYPE-TYPE SYSTEMS FACULTY OF SCIENCE, PALACKÝ UNIVERSITY, OLOMOUC RELATIONSHIPS OF PARAMETERS OF PLANETARY ORBITS IN SOLAR-TYPE SYSTEMS DOCTORAL THESIS PAVEL PINTR OLOMOUC 2013 VYJÁD ŘENÍ O PODÍLNICTVÍ Prohlašuji, že všichni auto ři se podíleli stejným dílem na níže uvedených článcích: Pintr P., Pe řinová V.: The Solar System from the quantization viewpoint. Acta Universitatis Palackianae, Physica, 42 - 43 , 2003 - 2004, 195 - 209. Pe řinová V., Lukš A., Pintr P.: Distribution of distances in the Solar System. Chaos, Solitons and Fractals 34 , 2007, 669 - 676. Pintr P., Pe řinová V., Lukš A.: Allowed planetary orbits. Chaos, Solitons and Fractals 36 , 2008, 1273 - 1282. Pe řinová V., Lukš A., Pintr P.: Regularities in systems of planets and moons. In: Solar System: Structure, Formation and Exploration . Editor: Matteo de Rossi, Nova Science Publishers, USA (2012), pp. 153-199. ISBN: 978-1-62100-057-0. Pintr P.: Závislost fotometrických parametr ů hv ězd na orbitálních parametrech exoplanet. Jemná Mechanika a Optika 11 - 12 , 2012, 317 - 319. Pintr P., Pe řinová V., Lukš A.: Areal velocities of planets and their comparison. In : Quantization and Discretization at Large Scales . Editors: Smarandache F., Christianto V., Pintr P., ZIP Publishing, Ohio, USA (2012), pp. 15 - 26. ISBN: 9781599732275. Pintr P., Pe řinová V., Lukš A., Pathak A.: Statistical and regression analyses of detected extrasolar systems. Planetary and Space Science 75 , 2013, 37 - 45. Pintr P., Pe řinová V., Lukš A., Pathak A.: Exoplanet habitability for stellar spectral classes F, G, K and M. 2013, v p říprav ě. -
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.