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Author : Paul E. Bauer
Publisher :
ISBN 13 :
Total Pages : 600 pages
Book Rating : 4.3/5 (91 download)
Download or read book Entry Vehicle Heating and Thermal Protection Systems written by Paul E. Bauer and published by . This book was released on 1983 with total page 600 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Aerospace Sciences Meeting. 20, 1982, Orlando, Fla..
Publisher :
ISBN 13 :
Total Pages : 556 pages
Book Rating : 4.:/5 (311 download)
Download or read book Entry Vehicle Heating and thermal protection systems: Space shuttle, solar starprobe, Jupiter Galileo probe written by Aerospace Sciences Meeting. 20, 1982, Orlando, Fla.. and published by . This book was released on 1983 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Committee on Reusable Launch Vehicle Technology and Test Program
Publisher : National Academies Press
ISBN 13 : 0309588960
Total Pages : 99 pages
Book Rating : 4.3/5 (95 download)
Download or read book Reusable Launch Vehicle written by Committee on Reusable Launch Vehicle Technology and Test Program and published by National Academies Press. This book was released on 1996-01-22 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt: The key to opening the use of space to private enterprise and to broader public uses lies in reducing the cost of the transportation to space. More routine, affordable access to space will entail aircraft-like quick turnaround and reliable operations. Currently, the space Shuttle is the only reusable launch vehicle, and even parts of it are expendable while other parts require frequent and extensive refurbishment. NASA's highest priority new activity, the Reusable Launch Vehicle program, is directed toward developing technologies to enable a new generation of space launchers, perhaps but not necessarily with single stage to orbit capability. This book assesses whether the technology development, test and analysis programs in propulsion and materials-related technologies are properly constituted to provide the information required to support a December 1996 decision to build the X-33, a technology demonstrator vehicle; and suggest, as appropriate, necessary changes in these programs to ensure that they will support vehicle feasibility goals.
Author :
Publisher :
ISBN 13 :
Total Pages : 204 pages
Book Rating : 4.:/5 (317 download)
Download or read book Thermal Protection Systems. Aspects of Thermal Protection of Interest to NASA and the Related Materials R and D Requirements written by and published by . This book was released on 1962 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (141 download)
Download or read book Entry Vehicle Heating and Thermal Protection Systems, Space Shuttle, Solar Starprobe, Jupiler Galileo Probe written by and published by . This book was released on 1983 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)
Download or read book Entry Thermal Protection written by and published by . This book was released on 1968 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : DONALD. TURRENTINE
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)
Download or read book Procedures for the Design of Thermal Protection Systems for Maneuverable Re-entry Vehicles written by DONALD. TURRENTINE and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Atmospheric re-entry of earth-orbital, hypersonic glide vehicles creates thermal problems. The heat affects not only the materials and construction of the airframe but also the crew and various subsystems of the vehicle. Successful solution of these problems depends upon the development of an effective thermal protective concept, which will also give the designer some latitude in his design philosophy. The role of the protective system is to significantly attenuate the influx of heat that is aerodynamically generated within the surrounding boundary layer. Attenuation is accomplished by combining external radiation shielding elements with backup insulation materials and an appropriate cooling system. Analytical procedures are presented for determining significant system parameters by transforming the differential heat conduction or diffusion equation into an algebraic expression by employing the calculus of finite differences. The adaptation of the resulting equation to digital computer programming is discussed, and numerical results are presented to indicate systems of minimum weight. (Author).
Author :
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)
Download or read book Entry Thermal Protection written by and published by . This book was released on 1968 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781721503872
Total Pages : 36 pages
Book Rating : 4.5/5 (38 download)
Download or read book Thermal Vacuum Facility for Testing Thermal Protection Systems written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-19 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: A thermal vacuum facility for testing launch vehicle thermal protection systems by subjecting them to transient thermal conditions simulating re-entry aerodynamic heating is described. Re-entry heating is simulated by controlling the test specimen surface temperature and the environmental pressure in the chamber. Design requirements for simulating re-entry conditions are briefly described. A description of the thermal vacuum facility, the quartz lamp array and the control system is provided. The facility was evaluated by subjecting an 18 by 36 in. Inconel honeycomb panel to a typical re-entry pressure and surface temperature profile. For most of the test duration, the average difference between the measured and desired pressures was 1.6% of reading with a standard deviation of +/- 7.4%, while the average difference between measured and desired temperatures was 7.6% of reading with a standard deviation of +/- 6.5%. The temperature non-uniformity across the panel was 12% during the initial heating phase (t less than 500 sec.), and less than 2% during the remainder of the test. Daryabeigi, Kamran and Knutson, Jeffrey R. and Sikora, Joseph G. Langley Research Center NASA/TM-2002-211734, NAS 1.15:211734, L-18163
Author : Kenneth A. Rathjen
Publisher :
ISBN 13 :
Total Pages : 202 pages
Book Rating : 4.:/5 (31 download)
Download or read book CAVE written by Kenneth A. Rathjen and published by . This book was released on 1977 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Adm Nasa
Publisher :
ISBN 13 : 9781730709555
Total Pages : 54 pages
Book Rating : 4.7/5 (95 download)
Download or read book Static and Aerothermal Tests of a Superalloy Honeycomb Prepackaged Thermal Protection System written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-11-02 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: A reusable metallic thermal protection system has been developed for vehicles with maximum surface temperatures of up to 2000 F. An array of two 12- by 12-in. panels was subjected to radiant heating tests that simulated Space Shuttle entry temperature and pressure histories. Results indicate that this thermal protection system, with a mass of 2.201 lbm/ft(exp 2), can successfully prevent typical aluminum primary structure of an entry vehicle like the Space Shuttle from exceeding temperatures greater than 350 F at a location on the vehicle where the maximum surface temperature is 1900 F. A flat array of 20 panels was exposed to aerothermal flow conditions, at a Mach number of 6.75. The panels were installed in a worst-case orientation with the gaps between panels parallel to the flow. Results from the aerothermal tests indicated that convective heating occurred from hot gas flow in the gaps between the panels. Proposed design changes to prevent gap heating occurred from hot gas flow in the gaps between the panels. Proposed design changes to prevent gap heating include orienting panels so that gaps are not parallel to the flow and using a packaged, compressible gap-filler material between panels to block hot gas flow in the gaps. Gorton, Mark P. and Shideler, John L. and Webb, Granville L. Langley Research Center...
Author : J Meseguer
Publisher : Elsevier
ISBN 13 : 0857096087
Total Pages : 413 pages
Book Rating : 4.8/5 (57 download)
Download or read book Spacecraft Thermal Control written by J Meseguer and published by Elsevier. This book was released on 2012-08-06 with total page 413 pages. Available in PDF, EPUB and Kindle. Book excerpt: Thermal control systems are an essential element of spacecraft design, ensuring that all parts of the spacecraft remain within acceptable temperature ranges at all times. Spacecraft thermal control describes the fundamentals of thermal control design and reviews current thermal control technologies. The book begins with an overview of space missions and a description of the space environment, followed by coverage of the heat transfer processes relevant to the field. In the third part of the book, current thermal control technologies are described, and in the final part, design, analysis and testing techniques are reviewed. - Provides background on the fundamentals of heat transfer which gives the reader a better understanding of the phenomenon and the way Space Thermal Control Systems work - Merges the experience of the authors in teaching aerospace engineering topics with the experience as compilers of the 'Spacecraft Thermal Control Design Data Handbook' of the European Space Agency and the development of in orbit thermal control systems for Spanish and ESA Missions - The engineering approach is enhanced with a full section on Thermal Control Design, Analysis and Testing
Author : Wilbur L. Hankey
Publisher : AIAA
ISBN 13 : 9781600861062
Total Pages : 160 pages
Book Rating : 4.8/5 (61 download)
Download or read book Re-Entry Aerodynamics written by Wilbur L. Hankey and published by AIAA. This book was released on 1988 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (317 download)
Download or read book Entry Gasdynamic Heating - Space Vehicle Design Criteria written by and published by . This book was released on 1971 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : IMechE
Publisher : Elsevier
ISBN 13 : 0857095056
Total Pages : 676 pages
Book Rating : 4.8/5 (57 download)
Download or read book Vehicle thermal Management Systems Conference and Exhibition (VTMS10) written by IMechE and published by Elsevier. This book was released on 2011-05-05 with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book contains the papers presented at the IMechE and SAE International, Vehicle Thermal Management Systems Conference (VTMS10), held at the Heritage Motor Centre, Gaydon, Warwickshire, 15-19th May 2011. VTMS10 is an international conference organised by the Automobile Division and the Combustion Engines and Fuels Group of the IMechE and SAE International. The event is aimed at anyone involved with vehicle heat transfer, members of the OEM, tier one suppliers, component and software suppliers, consultants, and academics interested in all areas of thermal energy management in vehicles. This vibrant conference, the tenth VTMS, addresses the latest analytical and development tools and techniques, with sessions on: alternative powertrain, emissions, engines, heat exchange/manufacture, heating, A/C, comfort, underhood, and external/internal component flows. It covers the latest in research and technological advances in the field of heat transfer, energy management, comfort and the efficient management of all thermal systems within the vehicle. - Aimed at anyone working in or involved with vehicle heat transfer - Covers research and technological advances in heat transfer, energy management, comfort and efficient management of thermal systems within the vehicle
Author : S. D. Williams
Publisher :
ISBN 13 :
Total Pages : 242 pages
Book Rating : 4.:/5 (317 download)
Download or read book Thermal Protection Materials written by S. D. Williams and published by . This book was released on 1992 with total page 242 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Sylvia M. Johnson
Publisher : BiblioGov
ISBN 13 : 9781289289089
Total Pages : 40 pages
Book Rating : 4.2/5 (89 download)
Download or read book Thermal Protection Materials for Reentry Applications written by Sylvia M. Johnson and published by BiblioGov. This book was released on 2013-08 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Thermal protection materials and systems (IRS) are used to protect spacecraft during reentry into Earth's atmosphere or entry into planetary atmospheres. As such, these materials are subject to severe environments with high heat fluxes and rapid heating. Catalytic effects can increase the temperatures substantially. These materials are also subject to impact damage from micrometeorites or other debris during ascent, orbit, and descent, and thus must be able to withstand damage and to function following damage. Thermal protection materials and coatings used in reusable launch vehicles will be reviewed, including the needs and directions for new materials to enable new missions that require faster turnaround and much greater reusability. The role of ablative materials for use in high heat flux environments, especially for non-reusable applications and upcoming planetary missions, will be discussed. New thermal protection system materials may enable the use of sharp nose caps and leading edges on future reusable space transportation vehicles. Vehicles employing this new technology would have significant increases in maneuverability and out-of-orbit cross range compared to current vehicles, leading to increased mission safety in the event of the need to abort during ascent or from orbit. Ultrahigh temperature ceramics, a family of materials based on HfB2 and ZrB2 with SiC, will be discussed. The development, mechanical and thermal properties, and uses of these materials will be reviewed.
