Books on the topic 'High pressure fuel system'
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Lattime, Scott B. Turbine engine clearance control systems: Current practices and future directions. National Aeronautics and Space Administration, Glenn Research Center, 2002.
Find full textJensen, Jørgen Arendt. A high-precision transducer measurement system. Electronics Laboratory, Electronics Institute, Technical University of Denmark, 1988.
Find full textLee, Henry. Space shuttle main engine high pressure fuel turbopump turbine blade cracking. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1988.
Find full textSouthward, James D. Laser doppler velocimetry in the space-shuttle main engine high-pressure fuel turbopump. Naval Postgraduate School, 1998.
Find full textAbdul-Aziz, Ali. Structural evaluation of a space main engine (SSME) high pressure fuel turbopump turbine blade. National Aeronautics and Space Administration, 1996.
Find full textAbdul-Aziz, Ali. Structural evaluation of a space main engine (SSME) high pressure fuel turbopump turbine blade. National Aeronautics and Space Administration, 1996.
Find full textAbdul-Aziz, Ali. Assessment of crack growth in a space shuttle main engine first-stage, high-pressure fuel turbopump blade. National Aeronautics and Space Administration, 1993.
Find full textChristie, Robert F. Browns Ferry Nuclear Plant variation in test intervals for high-pressure coolant injection (HPCI) system. Tennessee Valley Authority, 1985.
Find full textPaxson, Daniel E. A model for the space shuttle main engine high pressure oxidizer turbopump shaft seal system. National Aeronautics and Space Administration, 1991.
Find full textRutkowski, Richard J. Cold flow simulation of the alternate turbopump development turbine of the space shuttle main engine high pressure fuel turbopump. Naval Postgraduate School, 1994.
Find full textWong, S. High pressure coolant injection (HPCI) system risk-based inspection guide for Browns Ferry Nuclear Power Station. Division of Systems Safety and Analysis, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission, 1993.
Find full textMcKee, Joseph R. Experimental and computational investigation of cold-flow through the turbine of the space-shuttle main engine high-pressure fuel turbopump. Naval Postgraduate School, 1998.
Find full textHoward, Henry. A protest against the present high pressure system of education, as injurious to the mental and physical organization of youth. s.n.], 1987.
Find full textThe Chios gum mastic: A unique worldwide natural product aids diabetes, ulcers, cholesterol, high blood pressure, has anticancer properties, strengthens the immunisation system. J. Perikos, 1993.
Find full textW, Keeton L., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Space shuttle main engine high pressure fuel pump aft platform seal cavity flow analysis. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textW, Keeton L., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Space shuttle main engine high pressure fuel pump aft platform seal cavity flow analysis. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textParks, W. P. High pressure heat exchange system (HiPHES) for combined cycle power generation, phase I final report. U.S. Dept. of Energy, 1989.
Find full textL, Morgan Harry, United States. Army Aviation Research and Technology Activity., and Langley Research Center, eds. Pressure distribution data from tests of 2.29 M (7.5 ft.) span EET high-lift transport aircraft model in the Ames 12-foot pressure tunnel. National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textCenter, Huntsville Engineering, and United States. National Aeronautics and Space Administration., eds. Fluid flow analysis of the SSME high pressure fuel and oxidizer turbine coolant systems. Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center, 1990.
Find full textTurbine engine clearance control systems: Current practices and future directions. National Aeronautics and Space Administration, Glenn Research Center, 2002.
Find full textVelocity and pressure characteristics of a model SSME high pressure fuel turbopump: Final report. National Aeronautics and Space Administration, 1991.
Find full textSpace shuttle main engine high pressure fuel turbopump turbine blade cracking. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1988.
Find full textEnergy efficient engine: High-pressure compressor test hardware : detailed design report. National Aeronautics and Space Administration, 1988.
Find full textHigh pressure coolant injection (HPCI) system risk-based inspection guide. Division of Radiation Protection and Emergency Preparatness, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. SSME alternate turbopump development program: Design verification specification for high-pressure fuel turbopump. 3rd ed. United Technologies, Pratt & Whitney, 1989.
Find full textLaser Doppler Velocimetry in the Space-Shuttle Main Engine High-Pressure Fuel Turbopump. Storming Media, 1998.
Find full textUnited States. National Aeronautics and Space Administration., ed. An SSME high pressure oxidizer turboprop diagnostic system using G2tm real-time expert system. National Aeronautics and Space Administration, 1991.
Find full textAn SSME high pressure oxidizer turboprop diagnostic system using G2tm real-time expert system. National Aeronautics and Space Administration, 1991.
Find full textW, Shier, U.S. Nuclear Regulatory Commission. Division of Systems Safety and Analysis., and Brookhaven National Laboratory, eds. High pressure coolant injection system risk-based inspection guide for Hope Creek. Division of Systems Safety and Analysis, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission, 1992.
Find full textFocused Schlieren flow visualization studies of a multiple venturi fuel injectors in a high pressure combustor. National Aeronautics and Space Administration, 1994.
Find full textAssessment of the hydrogen external tank pressure decay anomaly on space transportation system (STS) 51-L. National Aeronautics and Space Administration, 1989.
Find full textAssessment of crack growth in a space shuttle main engine first-stage, high-pressure fuel turbopump blade. National Aeronautics and Space Administration, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. Assessment of crack growth in a space shuttle main engine first-stage, high-pressure fuel turbopump blade. National Aeronautics and Space Administration, 1993.
Find full textU.S. Nuclear Regulatory Commission. Division of Systems Safety and Analysis. and Brookhaven National Laboratory, eds. High pressure coolant injection system risk-based inspection guide for Hatch Nuclear Power Station. Division of Systems Safety and Analysis, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. Redesigned gas mass flow sensors for space shuttle pressure control system and fuel cell system: NASA contract no. NAS9-19322. National Aeronautics and Space Administration, 1996.
Find full textJ, Locke Randy, and NASA Glenn Research Center, eds. Non-intrusive, laser-based imaging of Jet-A fuel injection and combustion species in high pressure, subsonic flows. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textJ, Locke Randy, and NASA Glenn Research Center, eds. Non-intrusive, laser-based imaging of Jet-A fuel injection and combustion species in high pressure, subsonic flows. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textJ, Locke Randy, and NASA Glenn Research Center, eds. Non-intrusive, laser-based imaging of Jet-A fuel injection and combustion species in high pressure, subsonic flows. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textGeorge C. Marshall Space Flight Center., ed. Comprehensive structural dynamic analysis of the SSME/AT fuel pump first-stage turbine blade. National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.
Find full textUnited States. National Aeronautics and Space Administration., ed. FUEL INJECTOR PATTERNATION EVALUATION IN ADVANCED LIQUID-FUELED, HIGH PRESSURE, GAS TURBINE COMBUSTORS, USING... NASA/TM-1998-206292... APR. s.n., 1999.
Find full textUnited States. National Aeronautics and Space Administration., ed. Laser scanning system for pressure and temperature paints: Final report, NASA NCC2-5115. National Aeronautics and Space Administration, 1997.
Find full textUnited States. National Aeronautics and Space Administration., ed. Laser scanning system for pressure and temperature paints: Final report, NASA NCC2-5115. National Aeronautics and Space Administration, 1997.
Find full textLaser scanning system for pressure and temperature paints: Final report, NASA NCC2-5115. National Aeronautics and Space Administration, 1997.
Find full textR, Moes Timothy, Dryden Flight Research Facility, and AIAA Aerospace Sciences Meeting (29th : 1991 : Reno, Nevada), eds. The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system. NASA Ames Resarch Center, Dryden Flight Research Facility, 1991.
Find full textHigh-frequency data observations from space shuttle main engine low pressure fuel turbopump discharge duct flex joint tripod failure investigation. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.
Find full textExperimental and Computational Investigation of Cold-Flow Through the Turbine of the Space-Shuttle Main Engine High-Pressure Fuel Turbopump. Storming Media, 1998.
Find full textA, Farr R., and George C. Marshall Space Flight Center., eds. High-frequency data observations from space shuttle main engine low pressure fuel turbopump discharge duct flex joint tripod failure investigation. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.
Find full textA, Farr R., and George C. Marshall Space Flight Center., eds. High-frequency data observations from space shuttle main engine low pressure fuel turbopump discharge duct flex joint tripod failure investigation. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.
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