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Space Shuttle Main Engine Instrumented High Pressure Fuel Turbopump Technology Test Bed Testing Results Summary
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Book Synopsis Space Shuttle Main Engine Instrumented High Pressure Fuel Turbopump Technology Test Bed Testing Results Summary by : Mary E. Koelbl
Download or read book Space Shuttle Main Engine Instrumented High Pressure Fuel Turbopump Technology Test Bed Testing Results Summary written by Mary E. Koelbl and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Shuttle Main Engine Instrumented High Pressure Oxidizer Turbopump Technology Test Bed Testing Results Summary by : Mary E. Koelbl
Download or read book Space Shuttle Main Engine Instrumented High Pressure Oxidizer Turbopump Technology Test Bed Testing Results Summary written by Mary E. Koelbl and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technology Test Bed written by and published by . This book was released on 1991 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 1572 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. Congress. Senate. Committee on Commerce, Science, and Transportation. Subcommittee on Science, Technology, and Space Publisher : ISBN 13 : Total Pages :88 pages Book Rating :4.3/5 (91 download)
Book Synopsis Space Shuttle Main Engine Development Program by : United States. Congress. Senate. Committee on Commerce, Science, and Transportation. Subcommittee on Science, Technology, and Space
Download or read book Space Shuttle Main Engine Development Program written by United States. Congress. Senate. Committee on Commerce, Science, and Transportation. Subcommittee on Science, Technology, and Space and published by . This book was released on 1978 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. Congress. House. Committee on Science and Technology Publisher : ISBN 13 : Total Pages :558 pages Book Rating :4.F/5 ( download)
Book Synopsis Space Shuttle, 1978 by : United States. Congress. House. Committee on Science and Technology
Download or read book Space Shuttle, 1978 written by United States. Congress. House. Committee on Science and Technology and published by . This book was released on 1978 with total page 558 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722275013 Total Pages :26 pages Book Rating :4.2/5 (75 download)
Book Synopsis High-Frequency Data Observations from Space Shuttle Main Engine Low Pressure Fuel Turbopump Discharge Duct Flex Joint Tripod Failure Investigation by : National Aeronautics and Space Administration (NASA)
Download or read book High-Frequency Data Observations from Space Shuttle Main Engine Low Pressure Fuel Turbopump Discharge Duct Flex Joint Tripod Failure Investigation 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 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Observations made by Marshall Space Flight Center (MSFC) engineers during their participation in the Space Shuttle Main Engine (SSME) low pressure fuel turbopump discharge duct flex joint tripod failure investigation are summarized. New signal processing techniques used by the Component Assessment Branch and the Induced Environments Branch during the failure investigation are described in detail. Moreover, nonlinear correlations between frequently encountered anomalous frequencies found in SSME dynamic data are discussed. A recommendation is made to continue low pressure fuel (LPF) duct testing through laboratory flow simulations and MSFC-managed technology test bed SSME testing. Zoladz, T. F. and Farr, R. A. Marshall Space Flight Center ...
Download or read book 93-1885 - 93-1924 written by and published by . This book was released on 1992 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722755317 Total Pages :100 pages Book Rating :4.7/5 (553 download)
Book Synopsis Space Shuttle Main Engine Structural Analysis and Data Reduction/Evaluation. Volume 4 by : National Aeronautics and Space Administration (NASA)
Download or read book Space Shuttle Main Engine Structural Analysis and Data Reduction/Evaluation. Volume 4 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: The analysis performed on the Space Shuttle Main Engine (SSME) High Pressure Fuel Turbopump (HPFTP) inlet housings is summarized. Three DIAL finite element models were build to aid in assessing the structural life of the welds and fillets at the vanes. Complete results are given. Pool, Kirby V. Unspecified Center...
Book Synopsis Developmental Problems and Their Solution for the Space Shuttle Main Engine Alternate Liquid Oxygen High-pressure Turbopump: Anomaly Or Failure Investigation the Key by : R. S. Ryan
Download or read book Developmental Problems and Their Solution for the Space Shuttle Main Engine Alternate Liquid Oxygen High-pressure Turbopump: Anomaly Or Failure Investigation the Key written by R. S. Ryan and published by . This book was released on 1995 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Data analysis of the space shuttle main engine by : Ronald D. Flack
Download or read book Experimental Data analysis of the space shuttle main engine written by Ronald D. Flack and published by . This book was released on 1978 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental data analysis of the space shuttle main engine - high pressure oxidizer and fuel turbopumps by : Edgar J. Gunter
Download or read book Experimental data analysis of the space shuttle main engine - high pressure oxidizer and fuel turbopumps written by Edgar J. Gunter and published by . This book was released on 1979 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Test Results of the Highly Instrumented Space Shuttle Main Engine by : H. V. McConnaughey
Download or read book Test Results of the Highly Instrumented Space Shuttle Main Engine written by H. V. McConnaughey and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The dynamic analysis of the space shuttle main engine-high pressure fuel turbopump by : Edgar J. Gunter
Download or read book The dynamic analysis of the space shuttle main engine-high pressure fuel turbopump written by Edgar J. Gunter and published by . This book was released on 1976 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722755027 Total Pages :86 pages Book Rating :4.7/5 (55 download)
Book Synopsis Space Shuttle Main Engine Structural Analysis and Data Reduction/Evaluation. Volume 2 by : National Aeronautics and Space Administration (NASA)
Download or read book Space Shuttle Main Engine Structural Analysis and Data Reduction/Evaluation. Volume 2 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: The high-pressure oxidizer turbopump (HPOTP) consists of two centrifugal pumps, on a common shaft, that are directly driven by a hot-gas turbine. Pump shaft axial thrust is balanced in that the double-entry main inducer/impeller is inherently balanced and the thrusts of the preburner pump and turbine are nearly equal but opposite. Residual shaft thrust is controlled by a self-compensating, non-rubbing, balance piston. Shaft hang-up must be avoided if the balance piston is to perform properly. One potential cause of shaft hang-up is contact between the Phase 2 bearing support and axial spring cartridge of the HPOTP main pump housing. The status of the bearing support/axial spring cartridge interface is investigated under current loading conditions. An ANSYS version 4.3, three-dimensional, finite element model was generated on Lockheed's VAX 11/785 computer. A nonlinear thermal analysis was then executed on the Marshall Space Flight Center Engineering Analysis Data System (EADS). These thermal results were then applied along with the interference fit and bolt preloads to the model as load conditions for a static analysis to determine the gap status of the bearing support/axial spring cartridge interface. For possible further analysis of the local regions of HPOTP main pump housing assembly, detailed ANSYS submodels were generated using I-DEAS Geomod and Supertab (Appendix A). Sisk, Gregory A. Unspecified Center...
Book Synopsis Space Shuttle Technical Conference, Part 1 by :
Download or read book Space Shuttle Technical Conference, Part 1 written by and published by . This book was released on 1985 with total page 604 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Shuttle Main Engine Turbopump Transducer by : T. Peterson
Download or read book Space Shuttle Main Engine Turbopump Transducer written by T. Peterson and published by . This book was released on 1983 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: Advances in liquid rocket engine technology were required to meet the life and reuseability criteria set by the Space Shuttle Program for the Space Shuttle Main Engines (SSME). To verify the SSME design life, extensive development testing and hardware inspection was required. Each SSME has four turbopumps which are used to pump propellant for combustion. One of these turbopumps which pumps liquid oxygen is the High Pressure Oxygen Turbopump (HPPTP). Using a two-stage turbine, the HPOTP produces 29,410 horsepower to pump 69.6 pounds per second of liquid oxygen. One area of hardware inspection and testing to insure engine life and operation was in the area of the rocket engine turbopumps bearings. Bearing like is critical to the overall reusability of the HPOTP. After each development test of the SSME, inspection of many engine parts are made. During inspection of the HPOTP it was observed that some of the bearings in the pump were wearing excessively. The bearings in question were the number 3 and 4 bearings in the pump. To determine the cause of the wear, one HPOTP would be instrumented to monitor the bearing conditions.