Last edited by Mikagore
Tuesday, April 28, 2020 | History

2 edition of Some effects of thermal-cycle-induced deformation in rocket thrust chambers found in the catalog.

Some effects of thermal-cycle-induced deformation in rocket thrust chambers

Ned P Hannum

Some effects of thermal-cycle-induced deformation in rocket thrust chambers

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Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

    Subjects:
  • Rockets (Aeronautics) -- Launching,
  • Reusable space vehicles

  • Edition Notes

    StatementNed P. Hannum and Harold G. Price, Jr
    SeriesNASA technical paper -- 1834
    ContributionsPrice, Harold G, Lewis Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
    The Physical Object
    Pagination21 p. :
    Number of Pages21
    ID Numbers
    Open LibraryOL17979466M


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Some effects of thermal-cycle-induced deformation in rocket thrust chambers by Ned P Hannum Download PDF EPUB FB2

Some effects of thermal-cycle-induced deformation in rocket thrust chambers. Washington, D.C.: National Aeronautics and Space Administration, Scientific and.

Some effects of thermal-cycle-induced deformation in rocket thrust chambers eBook: National Aeronautics and Space Administration NASA: : Kindle Store Skip to main content. Try Prime Hello, Sign in Account & Lists Sign in Account & Lists Author: National Aeronautics and Space Administration NASA.

Buy Some effects of thermal-cycle-induced deformation in rocket thrust chambers (NASA technical paper) by Ned P Hannum (ISBN:) from Amazon's Book Author: Ned P Hannum. Ned P. Hannum has written: 'Some effects of thermal-cycle-induced deformation in rocket thrust chambers' -- subject(s): Rockets (Aeronautics), Launching, Reusable space vehicles 'Technology issues.

Some effects of thermal-cycle-induced deformation in rocket thrust chambers. Technical Report, NASA-TP, NASA () S., Quering, K. et al. Life prediction of thermally highly loaded components: modelling the damage process of a rocket combustion chamber hot wall.

CEAS Space J 1, 83 (). https Cited by: Handling and use of fluorine and fluorine-oxygen mixtures in rocket systems, (Washington: Scientific and Technical Information Division, Office of Technology Utilization, National Aeronautics and Space Administration; [for sale by the Supt.

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Filed under: Reusable space vehicles Reusable Launch Vehicle: Technology Development and Test Program, by National Research Council Aeronautics and Space Engineering Board (page images at NAP) The Lower Tiers of the Space Transportation Industrial Base (OTA-BP-ISS; Washington: GPO, ), by United States Congress Office of Technology.

In Europe, the concept of TMF-panel testing was first very successfully applied to rocket thrust chamber structures in the frame of the Ariane 5 Flight Recovery Programme in and We use cookies to make interactions with our website easy and meaningful, to better understand the use of our services, and to tailor advertising.

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Full text of "NASA Technical Reports Server (NTRS) Thermal Barrier Coating Workshop" See other formats. A technician inspects a 20,pound-thrust rocket engine used to investigate combustion instability, or screech, October Screech, a serious problem in rocket engines designed for the Apollo program, was investigated in the RETF using sub-scale models of injectors and thrust chambers.

NASA C Share & Embed. Embed Script. Size (px). Another Look at Rocket Thrust. ERIC Educational Resources Information Center.

Hester, Brooke; Burris, Jennifer. Rocket propulsion is often introduced as an example of. Rocket thrust chamber thermal barrier coatings. NASA Technical Reports Server (NTRS) Quentmeyer, R.

Subscale rocket thrust chamber tests were conducted to evaluate. 22 Oct - Velocity Burner Rigs. Suleyman A. Gokoglu, Case Western Reserve University, and West Palm Beach, Fl. Armstrong E.S. Test Program to Provide Confidence in Liquid Oxygen Cooling of Hydrocarbon Fueled Rocket Thrust Chambers.

NASA Technical Memorandum 12 p. Some Effects of Thermal-Cycle-Induced Deformation in Rocket Thrust Chambers. NASA TP, April 23 p. The evolution of water intake is also well matched (Figures 3d, 3e and 3f), some discrepancies at the end of the test have been attributed to small leakages in some of the very long term tests.

The evolutions of macrostructural and microstructural suctions at three different points (bottom, middle and top of the specimen) of test RS2E obtained. Full text of "NASA scientific and technical publications: A catalog of Special Publications, Reference Publications, Conference Publications, and Technical Papers, " See other formats.

PD APR PY VL 58 IS 2 BP EP DI /s PG 9 WC Zoology SC Zoology GA PB UT WOS ER PT J AU Glaz, B Friedmann, PP Liu, L Cajigas, JG Bain, J Sankar, LN AF Glaz, Bryan Friedmann, Peretz P. Liu, Li Cajigas, Juan G.

Bain, Jeremy Sankar, Lakshmi N. TI Reduced-Order Dynamic Stall Modeling with Swept. PREFACE The idea for the Handbook of Environmental Degradation of Materials originated several years ago when Bill Woishnis, the founder of William Andrew Publishing, and I met at my upstate New York office to discuss materials information needs at the practitioner level, an area that Bill and I had been involved in for some time.