1 edition of Re-entry and Planetary Entry Physics and Technology found in the catalog.
|Statement||Dynamics, Physics, Radiation, Heat Transfer and Ablation / by W. H. T. Loh ; edited by W. H. T. Loh|
|Series||Applied Physics and Engineering, An International Series -- 2, Applied Physics and Engineering, An International Series -- 2|
|The Physical Object|
|Format||[electronic resource] :|
|ISBN 10||364248929X, 3642489273|
|ISBN 10||9783642489297, 9783642489273|
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During the last decade, a rapid growth of knowledge in the field of re-entry and planetary entry has resulted in many significant advances useful to the student, engineer and scientist. The purpose of offering this course is to make available to them these recent significant advances in physics and technology.
During the last decade, a rapid growth of knowledge in the field of re-entry and planetary entry has resulted in many significant advances useful to the student, engineer and scientist.
The purpose of offering this course is to make available to them these recent significant advances in physics and : Paperback. Additional Physical Format: Online version: Loh, W.H.T. (Wellington Hsiao-tung), Re-entry and planetary entry physics and technology.
[New York] Springer-Verlag New York, Additional Physical Format: Online version: Loh, W.H.T. (Wellington Hsiao-tung), Re-entry and planetary entry. Berlin, Heidelberg, New York, Springer, Atmospheric entry is the movement of an object from outer space into and through the gases of an atmosphere of a planet, dwarf planet, or natural are two main types of atmospheric entry: uncontrolled entry, such as the entry of astronomical objects, space debris, or bolides; and controlled entry (or reentry) of a spacecraft capable of being navigated or.
Buy Re-entry and Planetary Entry Physics and Technology by W. Loh from Waterstones today. Click and Collect from your local Waterstones or get FREE UK delivery on orders over £Book Edition: Softcover Reprint of The Original 1st Ed. Propulsion Re-Entry Physics deals with the physics of propulsion re-entry and covers topics ranging from inductive magnetoplasmadynamic (MPD) propulsion systems to launch systems and orbiting maneuvering systems.
Problems of re-entry aerodynamics are considered, along with interaction problems in hypersonic fluid Edition: 1. Re-entry and Planetary Entry Physics and Technology: II / Advanced Concepts, Experiments, Guidance-Control and Technology Book 3 During the last decade, a rapid growth of knowledge in the field of re-entry and planetary entry has resulted in many significant advances useful to the student, engineer and scientist.
Entry, descent, and landing operations analysis for the Genesis re-entry capsule. 15th AAS/American Institute of Aeronautics and Astronautics Space Flight Mechanics Conference, paper AAS 05– Doenecke, J. and Elsner, M.
().Author: Andrew Ball, James Garry, Ralph Lorenz, Viktor Kerzhanovich. This book is organized into two parts encompassing nine chapters that highlight the re-entry vehicle design information and re-entry thermal protection and materials.
Part I deals first with a parametric study on the effects of initial conditions and various mass and aerodynamic parameters on the dynamic motion of a typical re-entry vehicle. Re-entry and Planetary Entry Physics and Technology: I / Dynamics, Physics, Radiation, Heat Transfer and Ablation Book 2 During the last decade, a rapid growth of knowledge in the field of re-entry and planetary entry has resulted in many significant advances useful to the student, engineer and scientist.
This book will appeal to students, practitioners, and research workers interested in propulsion re-entry and the accompanying physics. Show less Propulsion Re-Entry Physics deals with the physics of propulsion re-entry and covers topics ranging from inductive magnetoplasmadynamic (MPD) propulsion systems to launch systems and orbiting.
If the re-entry velocity is km/s and the re-entry flight-path angle is 10 degrees, determine the maximum deceleration it will experience and at what altitude.
The capsule’s BC is kg/m^2 Homework Equations a max = V^2 re-entry b sin y/ 2e The Attempt at a Solution a max = m/s^2 (m^-1 sin(10)) / 2(). An historical perspective of re-entry issues is presented, and factors that determine the flight profiles of re-entry vehicles are considered.
An outline is given of the aerothermal environment. Dynamics of Atmospheric Re-Entry Frank J Regan, Satya M Anandakrishnan Presenting comprehensive coverage of the dynamics of atmospheric re-entry, this text details fundamental concepts and practical applications such as the atmospheric model and re-entry mechanics, and goes on to discuss specific topics such as re-entry decoys, flow fields and.
1 The energy which a moving object possesses because of its motion. 2 More than double because to lift the extra fuel requires yet more fuel.
3 Put another way, the average rate at which the space shuttle dissipates energy throughout its re-entry is rather higher than the rate at which Houston consumes energy in the same period. That isn't Houston as in Mission Control.
Relaxation in Shock Waves by Y. Stupochenko,available at Book Depository with free delivery worldwide. Dynamics of Atmospheric Re-Entry. The Planetary Entry Systems Synthesis Tool: A conceptual design and analysis tool for EDL systems.
Analytic Hypersonic Aerodynamics for Conceptual Design of Entry Vehicles. Journal of Mechanical Science and Technology, Vol. 20, No. Arc Physics by Max F.
Re-entry and Planetary Entry Physics and Technology. Loh. 23 Aug Paperback. US$ Add to basket. Relaxation in Shock Waves. New Problems of Re-entry Aerodynamics RADIATING FLOWS DURING ENTRY INTO PLANETARY ATMOSPHERES by R.
GOULARD, R. BOUGHNER, R. BURNS and H. NELSON Purdue University, Lafayette, Indiana (U.S.A.) 1. Introduction During the past 3 years, new feats of space exploration have added to our knowledge of the by: 6.
Skip to Main ContentAuthor: Sarag J. Saikia, Jeffrey F. Rhoads, James M. Longuski. Hypersonic meteoroid entry physics (HyMEP) is a subject of continuous interest, either for understanding the relevant fluid-dynamics phenomenology (see chapters 6, 7, 9 and 10) or to study the composition of the fragments coming from the meteoroid–Earth impact containing primordial elements characterizing the life of the Universe (chapters 2–5 and 11).
The Stardust sample return probe had an interesting re-entry to Earth's atmosphere. Returning from a solar orbit the maximum deceleration has been reported as 34g. Maximum temperatures are estimated at around 3, Kelvin or degrees C at the surface. It should be noted that the entry probe had no re-entry data recording so this measurement was estimated from.
Download Citation | Atmospheric Re-Entry Vehicle Mechanics | Ballistic reentry vehicles, capsules and planetary probes are the fastest human designed objects to fly through planet's : Patrick Gallais. Atmospheric entry is the movement of an object from outer space into and through the gases of an atmosphere of a planet, dwarf planet or natural satellite.
There are two main types of atmospheric entry: uncontrolled entry, such as the entry of astronomical objects, space debris or bolides; and controlled entry (or reentry) of a spacecraft capable of being navigated or.
Re-entry and Planetary Entry Physics and Technology. Find all books from W.H.T. Loh; W.H.T. Loh. At you can find used, antique and new books, compare results and immediately purchase your selection at the best price. [PU: Springer, Berlin/Heidelberg/New York, NY] Re-entry Brand: Springer Science+Business Media.
What Newton did to simplify the planetary motions must now be done to unite in one whole the various isolated theories of mathematical physics.: In the early twenty-first century, satellites and planetary probes are routinely shot into space on multistage rockets.: The story is that huge earthquakes are ripping earth apart, and a planetary evacuation needs to be set underway.
Yes, she’s a little worse for wear, isn’t she. But then again, that’s what atmospheric re-entry and °Celsius ( °Fahrenheit) worth of heat will do to you. Such was the state of the. The present volume is organized into four chapters that highlight recent progress in the following areas of re-entry research: low-density phenomena at hypersonic flow conditions, high temperature kinetics and transport properties, aerothermal ground simulation and measurements, and numerical simulations of hypersonic flows.
Aircraft Control Allocation Wayne Durham, Virginia Polytechnic Institute and State University, USA Kenneth A. Bordignon, Embry-Riddle Aeronautical University, USA Roger Beck, Dynamic Concepts, Inc., USA An authoritative work on aircraft control allocation by its pioneers Aircraft Control Allocation addresses the problem of allocating supposed redundant flight controls.
Obtained BS, Massachusetts Institute of Technology (MIT), Cambridge (Mass.). Obtained MS, Massachusetts Institute of Technology (MIT), Cambridge (Mass.). – Consultant on Re-entry Physics, Lockheed Missiles and Space Company.
– Research Assistant, Institute for Plasma Research, Stanford University, Stanford (Calif. Buy Atmospheric Re-entry Vehicle Mechanics by Gallais, Patrick (ISBN: ) from Amazon's Book Store. Everyday low prices and free delivery on eligible orders.3/5(1). He discusses the fundamentals of hypersonic aerodynamics as they are used in estimating the aerodynamic characteristics of re-entry configurations, re-entry heat transfer for both lifting (space shuttle) and ballistic (Apollo) configurations, thermal protection systems, and the application of high-temperature materials in design.
Prof. Sivaram is with the Indian Institute of Astrophysics, Bangalore, India, specializing in theoretical astrophysics and cosmology. He has made seminal contributions to fundamental interactions in the early universe and high energy astrophysics, among them the origin and acceleration of cosmic rays and gamma rays, neutrino production in quasars, neutron 2/5(1).
F.J. Regan and S.M. Anandakrishnan, Dynamics of Atmospheric Re-Entry, AIAA, W.T. Thomson, Introduction to Space Dynamics, Sputnik Explorer Vanguard Astronautics Missile defense Baikonur Tyuratam Rocket equation.
The capability to experimentally reproduce the atmospheric re-entry in terms of mechanical and thermal stresses is a crucial point for manned or unmanned aerospace missions as well as for the study of the re-entry phenomena of any objects de-orbiting or entering the Earth's atmosphere, due to the complex physical and chemical phenomena that.
rockets, re-entry, GNC precise orbits space debris transfer orbits planetary expl. & astr. prop. + optim. x x x x numericalastrodyn. x x x x rocketmotion x x re-entry systems x x x x satelliteorbitdet.
x x x x planetary sciences II x x mission geometry x x x x x spaceinstrumentation x2 thermal rocket prop.
x1 s/c att. dyn& control x1 special. A typical re-entry capsule is designed using computational design software and it is imported to a computational fluid dynamics solver and flow simulations are done at various input conditions.
Stanford University unstructured computational fluid dynamics solver is used for this purpose to solve complex, multiphysics analysis, and optimization Author: J Bruce Ralphin Rose, P Saranya, JV Bibal Benifa.
atmospheric re-entry the return to an atmosphere previously left for space. Often the word atmospheric is dropped and the term re-entry (or reentry) is taken to mean atmospheric re-entry in context. augered-in after EDL (Entry, Decent and Landing) or TPS (Thermal Protection System) failure, the entry vehicle is said to have augered-in.
Facing the Heat Barrier: A History of Hypersonics. Heppenheimer. Facing the Heat Barrier: A History of Hypersonics. Heppenheimer. Hypersonics is the study of flight at speeds where. aerodynamic heating dominates the physics of the problem. Typically this is Mach 5 and higher. Hypersonics is an engineering science with closeFile Size: 1MB.
The Mechanical Universe Series by PBS: This is an excellent series produced by Public Broadcasting, JPL lab and the California Institute of Technology. Each one of these 52 films is 30 minutes long so they require almost an entire class period to show the whole thing, however you may also cue up the video and show only the part you desire.I thought one way of re-entry was via a highly elliptical orbit: The perigee gets low enough (app.
km) to reach into the atmosphere and then re-entry happens. Things yet don't seem to be that simple from what my observations of D tell me: I started observing it a month ago, when its apogee was at km, perigee at 99 km.