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High Temperature Test Facility At The Nasa Lewis Engine Components Research Laboratory
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722278915 Total Pages :24 pages Book Rating :4.2/5 (789 download)
Book Synopsis High-Temperature Test Facility at the NASA Lewis Engine Components Research Laboratory by : National Aeronautics and Space Administration (NASA)
Download or read book High-Temperature Test Facility at the NASA Lewis Engine Components Research Laboratory written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-05 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: The high temperature test facility (HTTF) at NASA-Lewis Engine Components Research Laboratory (ECRL) is presently used to evaluate the survivability of aerospace materials and the effectiveness of new sensing instrumentation in a realistic afterburner environment. The HTTF has also been used for advanced heat transfer studies on aerospace components. The research rig uses pressurized air which is heated with two combustors to simulate high temperature flow conditions for test specimens. Maximum airflow is 31 pps. The HTTF is pressure rated for up to 150 psig. Combustors are used to regulate test specimen temperatures up to 2500 F. Generic test sections are available to house test plates and advanced instrumentation. Customized test sections can be fabricated for programs requiring specialized features and functions. The high temperature test facility provides government and industry with a facility for testing aerospace components. Its operation and capabilities are described. Colantonio, Renato O. Glenn Research Center RTOP 505-62-3B...
Book Synopsis High-temperature Test Facility at the NASA Lewis Engine Components Research Laboratory by :
Download or read book High-temperature Test Facility at the NASA Lewis Engine Components Research Laboratory written by and published by . This book was released on 1990 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aeropropulsion Facilities at the NASA Lewis Research Center by : Lewis Research Center
Download or read book Aeropropulsion Facilities at the NASA Lewis Research Center written by Lewis Research Center and published by . This book was released on 1995 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Book Synopsis Space Chemical Propulsion Test Facilities at NASA Lewis Research Center by : Donald C. Urasek
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Book Synopsis Scientific and Technical Aerospace Reports by :
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Book Synopsis NASA Lewis Research Center's Combustor Test Facilities and Capabilities by : Jean Bianco
Download or read book NASA Lewis Research Center's Combustor Test Facilities and Capabilities written by Jean Bianco and published by . This book was released on 1995 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781792696824 Total Pages :28 pages Book Rating :4.6/5 (968 download)
Book Synopsis NASA Lewis Research Center's Preheated Combustor and Materials Test Facility by : National Aeronautics and Space Adm Nasa
Download or read book NASA Lewis Research Center's Preheated Combustor and Materials Test Facility written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-12-29 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Preheated Combustor and Materials Test Facility (PCMTF) in the Engine Research Building (ERB) at the NASA Lewis Research Center is one of two unique combustor facilities that provide a nonvitiated air supply to two test stands, where the air can be used for research combustor testing and high-temperature materials testing. Stand A is used as a research combustor stand, whereas stand B is used for cyclic and survivability tests of aerospace materials at high temperatures. Both stands can accommodate in-house and private industry research programs. The PCMTF is capable of providing up to 30 lb/s (pps) of nonvitiated, 450 psig combustion air at temperatures ranging from 850 to 1150 g F. A 5000 gal tank located outdoors adjacent to the test facility can provide jet fuel at a pressure of 900 psig and a flow rate of 11 gal/min (gpm). Gaseous hydrogen from a 70,000 cu ft (CF) tuber is also available as a fuel. Approximately 500 gpm of cooling water cools the research hardware and exhaust gases. Such cooling is necessary because the air stream reaches temperatures as high as 3000 deg F. The PCMTF provides industry and Government with a facility for studying the combustion process and for obtaining valuable test information on advanced materials. This report describes the facility's support systems and unique capabilities. Nemets, Steve A. and Ehlers, Robert C. and Parrott, Edith Glenn Research Center NASA-TM-106676, E-9012, NAS 1.15:106676 NAS3-27186; RTOP 505-62-84...
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Book Synopsis Hot Corrosion Test Facility at the NASA Lewis Special Projects Laboratory by :
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Book Synopsis Aeronautics and Space Report of the President by : United States. President
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Book Synopsis Aeronautics and Space Report of the President ... Activities by : United States. President
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