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Saturday, May 9, 2020 | History

2 edition of Thermophysics and temperature control of spacecraft and entry vehicles found in the catalog.

Thermophysics and temperature control of spacecraft and entry vehicles

G. B. Heller

Thermophysics and temperature control of spacecraft and entry vehicles

by G. B. Heller

  • 399 Want to read
  • 8 Currently reading

Published by Academic .
Written in English


Edition Notes

Statementedited by G.B. Heller.
SeriesProgress in astronautics and aeronautics -- v.18
ContributionsAmerican Institute of Aeronautics and Astronautics.
ID Numbers
Open LibraryOL19808358M

Progress in Astronautics and Aeronautics, Volume Thermal Design Principles of Spacecraft and Entry Bodies is a collection of technical papers drawn mainly from the American Institute of Aeronautics and Astronautics Third Thermophysics Specialist Conference, held in Los Angeles, California on June , This volume is divided into. A modest level of control is achieved with an uncontrolled, passive reservoir. Precision control is achievable with a temperature controlled reservoir. Axial groove capillary wick structures are often utilized because of the relative ease of manufacturing and their demonstrated reliability in spacecraft and instrument thermal control applications.

Part of the Advances in Cryogenic Engineering book series (ACRE, volume 14) Abstract Due to the rapid growth of cryogenic technology and the accompanying rise in the use of high vacuum insulation, thermal radiation of metais at cryogenic temperatures has become an area of increasing by: 9. specified operating conditions. Spacecraft operating conditions were normally rather broad (plus or minus 20 to 30 OC) and power levels were low (in the 10's to 's of Watts), and such simple techniques worked well enough. However, modem spacecraft and instruments are requiring much tighter temperature control (to a 1/10' OC) over.

By obtaining aerothermal heating flight data at Mars, understanding how to efficiently use elaborate quantum chemistry data in production design tools, and investigating the physics of meteor entry in high-enthalpy ground tests, the ability to validate complex thermophysics models is greatly improved. The Thermophysics Facilities Branch (TSF) is responsible for the safe, effective, and efficient operation of the TS Division’s high enthalpy facilities. TSF facilities provide unique environmental simulation capability to serve customer-driven aerothermal and thermal response simulation requirements for NASA’s mission directorates.


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Thermophysics and temperature control of spacecraft and entry vehicles by G. B. Heller Download PDF EPUB FB2

Progress in Astronautics and Aeronautics, Volume Thermophysics and Temperature Control of Spacecraft and Entry Vehicles is a selection of technical papers based on two American Institute of Aeronautics and Astronautics meetings, namely, The Thermophysics Specialist Conference, held in Monterey, California on Septemberand the Third Aerospace.

The papers in this volume, encompassing a number of specialized scientific disciplines, cover some of the most important problems of contemporary thermophysics research and technology. They will be of value to scientists and engineers concerned with spacecraft thermal design and control, and evaluation of thermal radiation properties of materials.

Progress in Astronautics and Aeronautics, Volume Thermophysics and Temperature Control of Spacecraft and Entry Vehicles is a selection of technical papers based on two American Institute of Aeronautics and Astronautics meetings, namely, The Thermophysics Specialist Conference, held in Monterey, California on Septemberand the Third Book Edition: 1.

Thermophysics and temperature control of spacecraft and entry vehicles. New York: Academic Press, (DLC) Material Type: Conference publication, Document, Internet resource: Document Type: Internet Resource, Computer File: All Authors / Contributors: Gerhard B Heller; American Institute of Aeronautics and Astronautics.

Thermophysics and temperature control of spacecraft and entry vehicles; a selection of technical papers. Progress in Astronautics and Aeronautics, Volume Thermophysics and Temperature Control of Spacecraft and Entry Vehicles is a selection of technical papers based on two American Institute of Aeronautics and Astronautics meetings, namely, The Thermophysics Specialist Conference, held in Monterey, California on Septemberand the.

Thermophysics is characterized also by the exactness with which solutions are demanded, especially in the application to temperature control of spacecraft during long flights and to the questions of survival of re-entry bodies upon entering the.

Power Systems for Space Flight - Ebook written by Morris Zipkin. Read this book using Google Play Books app on your PC, android, iOS devices. Download for offline reading, highlight, bookmark or take notes while you read Power Systems for Space Flight.

Progress in Astronautics and Aeronautics, Volume Thermal Design Principles of Spacecraft and Entry Bodies is a collection of technical papers drawn mainly from the American Institute of Aeronautics and Astronautics Third Thermophysics Specialist Conference, held in Los Angeles, California on JuneThis volume is divided into three parts.

Progress in Astronautics and Aeronautics, Volume Thermophysics of Spacecraft and Planetary Bodies: Radiation Properties of Solids and the Electromagnetic Radiation Environment in Space is a collection of technical papers drawn mainly from the American Institute of Aeronautics and Astronautics Thermophysics Specialist Conference, held in New Orleans on.

Spacecraft radiative transfer and temperature control: technical papers from the AIAA 19th aerospace sciences meeting, January [St. Louis, Mo.], and the AIAA 16th thermophysics conference, June [Palo Alto, Calif.] Horton, Thomas E.

Progress in Astronautics and Aeronautics, Volume Thermophysics of Spacecraft and Planetary Bodies: Radiation Properties of Solids and the Electromagnetic Radiation Environment in Space is a collection of technical papers drawn mainly from the American Institute of Aeronautics and Astronautics Thermophysics Specialist Conference, Book Edition: 1.

Thermophysics and Temperature Control of Spacecraft and Entry Vehicles. Gerhard B. Heller Elsevier Inc. Thermophysics of Spacecraft and Planetary Bodies: Radiation Properties of Solids and the Electromagnetic Radiation Environment [Heller, Gerhard B., Ed] on *FREE* shipping on qualifying offers.

Thermophysics of Spacecraft and Planetary Bodies: Radiation Properties of Solids and the Electromagnetic Radiation EnvironmentAuthor: Ed Heller, Gerhard B. Spacecraft Thermal Control Systems Col.

John E. Keesee Lesson Objectives: 1. The student will understand thermal control processes 2. The student will be able to calculate thermal balances and equilibrium temperatures 3. The student will be File Size: KB.

Similar Items. Thermal design principles of spacecraft and entry bodies Published: () ; Entry vehicle heating and thermal protection systems Space Shuttle, Solar Starprobe, Jupiter Galileo Probe / Published: () Thermophysics and temperature control of spacecraft and entry vehicles Published: ().

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.

The heat pipes most commonly used on spacecraft are an aluminium/ammonia type that allows optimal temperature control in the °C range. Since the quantity of heat transported by the pipe is defined by its design and dimensions, the equivalent thermal conductance is fixed, leading to the Constant Conductance Heat Pipe (CCHP in Fig.

6a). Tiefgekühlt und doch nicht haltbar. Das Lebensmitteldiktat der Konzerne by Gerhard, Häußler, Heller, Peter und Rosenberger, Christel: and a great selection of related books, art and collectibles available now at Spacecraft Radiative Transfer and Temperature Control Paas83 (Progress in astronautics and aeronautics) First Edition by T.

Horton (Editor) ISBN ISBN Why is ISBN important. ISBN. This bar-code number lets you verify that you're getting exactly the right version or edition of a book. AIAA Preliminary Thermal Analysis of a Mars Sample Return Earth Entry Vehicle Ruth M. Amundsen, John A.

Dec, Robert A. Mitcheltree, Michael C. Lindell, Robert A. Dillman NASA Langley Hampton, VA 34th AIAA Thermophysics Conference June / Denver, CO I.A 'read' is counted each time someone views a publication summary (such as the title, abstract, and list of authors), clicks on a figure, or views or downloads the full-text.In: Thermophysics and Thermal Control (R.

Visjanta, ed.) Vol of Progress in Astronautics and Aeronautics, American Institute of Aeronautics and Astronautics (Presented as Paper 78– at the 2nd American Institute of Aeronautics and Astronautics/ASME Thermophysics and Heat Transfer Conference, Palo Alto, California, May 24–26, ).Author: Andrew Ball, James Garry, Ralph Lorenz, Viktor Kerzhanovich.