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Fuel pumps

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• Automobiles -- Motors
• Internal combustion engines
• Pumping machinery

• Internal combustion engines -- Fuel systems

• Fuel pumps -- Handbooks, manuals, etc.
• Fuel pumps -- Maintenance and repair
• Fuel pumps -- Testing
• Automobiles -- Fuel systems
• Diesel motor -- Fuel systems
• Motor vehicles -- Fuel systems
• Rocket engines -- Fuel systems

• Fuel injection pumps

• Fuel injection systems. (Diesel Publications, 1956), by Diesel equipment superintendent, Brian P. Emerson, and inc Diesel Publications (page images at HathiTrust)
• Fuel injection systems (Diesel Publications, 1950), by Diesel Power & Diesel Transportation, Brian P. Emerson, and inc Diesel Publications. (page images at HathiTrust)
• Liquid rocket engine turbopump rotating-shaft seals (National Aeronautics and Space Administration, 1978), by R. E. Burcham and Russell B. Keller (page images at HathiTrust)
• 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), by S. A. Lowry, L. W. Keeton, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Fuel injection pumps and nozzles, workers of American Bosch Division, AMBAC Industries, Inc., Springfield, Mass. : report to the President on investigation no. TEA-W-81 under section 301(c)(2) of the Trade Expansion Act of 1962. (U.S. Tariff Commission, 1971), by United States Tariff Commission (page images at HathiTrust)
• Effect of ratio of wall boundary-layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream (National Aeronautics and Space Administration ;, 1974), by Charles R. McClinton and Langley Research Center (page images at HathiTrust)
• Some injector element detail effects on screech in hydrogen-oxygen rockets (National Aeronautics and Space Administration ;, 1974), by Ned P. Hannum and Lewis Research Center (page images at HathiTrust)
• Drag and distribution measurements of single-element fuel injectors for supersonic combustors (National Aeronautics and Space Administration ;, 1974), by Louis A. Povinelli and Lewis Research Center (page images at HathiTrust)
• Effect of interjet spacing on mixing of multiple coaxial jets in supersonic flow (National Aeronautics and Space Administration ;, 1974), by A. K. Lorber, Joseph A. Schetz, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Investigation of spray for characteristics for flashing injection of fuels containing dissolved air and superheated fuels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), by A. S. P. Solomon, G. M. Faeth, L-D. Chen, Pennsylvania State University, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
• Nonreactive mixing study of a scramjet swept-strut fuel injector (National Aeronautics and Space Administration ;, 1975), by Charles R. McClinton and Langley Research Center (page images at HathiTrust)
• Experimental investigation of a swept-strut fuel-injector concept for scramjet application (National Aeronautics and Space Administration ;, 1977), by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of predicted and experimental cavitation performance of 84 ̊helical inducer in water and hydrogen (National Aeronautics and Space Administration ;, 1970), by George Kovich and Lewis Research Center (page images at HathiTrust)
• Design and evaluation of an oxidant-fuel-ratio-zoned rocket injector for high performance and ablative engine compatibility (National Aeronautics and Space Administration ;, 1972), by Jerry M. Winter, Arthur M. Shinn, Albert J. Pavli, and Lewis Research Center (page images at HathiTrust)
• Aerodynamic drag and fuel spreading measurements in a simulated scramjet combustion module (National Aeronautics and Space Administration ;, 1974), by Louis A. Povinelli and Lewis Research Center (page images at HathiTrust)
• Investigation of a liquid-fluorine inducer and main-stage pump combination designed for a suction specific speed of 20000 (National Aeronautics and Space Administration ;, 1965), by Walter Martin Osborn and Lewis Research Center (page images at HathiTrust)

• Operator, organizational, direct support, and general support maintenance manual for tester, fuel injector pump : single end drive, 150 to 3600 RPM (4910-01-037-9417) and adapter kits, fuel injector : American Bosch APE-6BB (4910-01-005-2850), American Bosch PSB-6A and PSB-6 (4910-01-005-2851), American Bosch PSB-12BT (4910-01-005-2852), Simmonds SU (4910-01-005-2853), International Harvester 3200 (4910-01-006-3073), American Bosch PSJ-6A (4910-01-006-3072), Caterpillar (4910-01-005-2854), Roosa Master (4910-01-005-2855), and Cummins (4910-00-763-7495). (Headquarters, Dept. of the Army, 1982), by United States. Department of the Army (page images at HathiTrust)
• Organizational direct support, and general support maintenance repair parts and special tools list for tester, fuel injector pump : single end drive, 150 to 3600 RPM (4910-01-037-9417) and adapter kits, fuel injector : American Bosch APE-6BB (4910-01-005-2850), American Bosch PSB-6A and PSB-6 (4910-01-005-2851), American Bosch PSB-12BT (4910-01-005-2852), Simmonds SU (4910-01-005-2853), International Harvester 3200 (4910-01-006-3073), American Bosch PSJ-6A (4910- 01-006-3072), Caterpillar (4910-01-005-2854), Roosa Master (4910-01-005-2855), and Cummins (4910-00-763-7495). (Headquarters, Dept. of the Army, 1982), by United States. Dept. of the Army (page images at HathiTrust)
• Fuel pumps. (Departments of the Army and the Air Force, 1989), by United States Department of the Air Force and United States. Department of the Army (page images at HathiTrust)

• Operator and organizational maintenance manual (including repair parts and spoecial tool lists) : tester, diesel fuel injector nozzle (Bacharach Industrial Instrument Company model YFL) (4910-255-8641) with connector set 44 (Bacharach part number 65-275) (4910-955-5517) and connector set (ORD DWG B11020498) (4910-955-5516). (Headquarters, Dept. of the Army, 1989), by United States. Department of the Army (page images at HathiTrust)
• Operator, organizational, direct support, and general support maintenance manual for tester, fuel injector pump : single end drive, 150 to 3600 RPM (4910-01-037-9417) and adapter kits, fuel injector : American Bosch APE-6BB (4910-01-005-2850), American Bosch PSB-6A and PSB-6 .... (Headquarters, Dept. of the Army, 1990), by United States. Department of the Army (page images at HathiTrust)
• Direct support and general support maintenance manual (including repair parts and special tools list) for pump, fuel, metering and distributing, assembly 2910-178-1185, 2910-759-5410, 2910-908-6320, 2910-968-6317, and 2910-116-8241. (Headquarters, Dept. of the Army, 1990), by United States. Department of the Army (page images at HathiTrust)
• Direct support and general support maintenance manual (including direct support, general support, and depot maintenance repair parts and special tools list) : pump, fuel metering and distributing American Bosch model PSB-12BT NSN 2910-01-073-0124. (Headquarters, Dept. of the Army, 1984), by United States. Department of the Army (page images at HathiTrust)

• Centaur space vehicle pressurized propellant feed system tests. (National Aeronautics and Space Administration ;, 1972), by Lewis Research Center (page images at HathiTrust)
• Exploratory tests of two strut fuel injectors for supersonic combustion (National Aeronautics and Space Administration ;, 1974), by Griffin Y. Anderson, Paul B. Gooderum, and Langley Research Center (page images at HathiTrust)

• Replacing Gasoline: Alternative Fuels for Light-Duty Vehicles (OTA-E-364; 1990), by United States Congress Office of Technology Assessment (page images at HathiTrust)
• The Association of automotive fuel composition with exhaust reactivity (U.S. Dept. of Interior, Bureau of Mines, 1973), by C. J. Raible, G. P. Sturm, B. H. Eccleston, Basil Dimitriades, Bartlesville Energy Research Center, United States Environmental Protection Agency, and United States Bureau of Mines (page images at HathiTrust)
• Saving gasoline and increasing mileage by proper carburetor adjustment (U.S. Dept. of the Interior, Bureau of Mines, 1924), by G. W. Jones, A. A. Straub, and United States Bureau of Mines (page images at HathiTrust)
• Gasoline saved on government trucks by adjusting carburetors by exhaust gas analysis (U.S. Dept. of the Interior, Bureau of Mines, 1923), by G. W. Jones, Arno Carl Fieldner, and United States Bureau of Mines (page images at HathiTrust)

• Diesel-engine construction, fuel systems (International Textbook Co., 1948), by International Correspondence Schools (page images at HathiTrust)
• Fuel injection pumps and nozzles, workers of American Bosch Division, AMBAC Industries, Inc., Springfield, Mass. : report to the President on investigation no. TEA-W-81 under section 301(c)(2) of the Trade Expansion Act of 1962. (U.S. Tariff Commission, 1971), by United States Tariff Commission (page images at HathiTrust)

• Concours International de Moteurs et Appareils Utilisant l'Alcool Dénaturé Ayant eu Lieu à Paris en Mai 1902: Rapports des Jurys (in French; Paris: Imp. Nationale, 1902), contrib. by Max Ringelmann, L. Lindet, E. Sorel, and H. De la Valette
  • multiple formats at Google; US access only
  • multiple formats at archive.org; some illustrations and figures omitted
  • page images at HathiTrust; US access only
• Guide to alternative fuel vehicles (California Energy Commission, 1999), by McKinley Addy and California Energy Commission. Transportation Technology & Fuels Office (page images at HathiTrust)
• Transportation technology status report (California Energy Commission, 1997), by Tom MacDonald and California Energy Commission. Technology Evaluation Office (page images at HathiTrust)
• Evaluation of compressed natural gas (CNG) fueling systems (California Energy Commission, 1999), by South Coast Air Quality Management District (Calif.). Technology Advancement Office, California Energy Commission. Transportation Technology & Fuels Office, and Inc ARCADIS Geraghty & Miller (page images at HathiTrust)

• 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), by S. A. Lowry, L. W. Keeton, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Measurements of the extinction parameters of hot seeded hydrogen at high pressures (National Aeronautics and Space Administration ;, 1971), by J. Richard Williams, J. D. Clement, W. L. Partain, Lewis Research Center, and Georgia Institute of Technology (page images at HathiTrust)
• Analysis of the measured effects of the principal exhaust effluents from solid rocket motors (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by R. Dawbarn, D. J. Watson, Max Kinslow, Arnold Engineering Development Center, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Performance investigation of a nonpumping rocket-ejector system for altitude simulation (National Aeronautics and Space Administration, 1959), by Anthony Fortini and Lewis Research Center (page images at HathiTrust)
• Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. II, Overall two-stage performance (National Aeronautics and Space Administration ;, 1966), by Richard J. Roelke, David G. Evans, Roy G. Stabe, and Lewis Research Center (page images at HathiTrust)
• Comparison of predicted and experimental cavitation performance of 84 ̊helical inducer in water and hydrogen (National Aeronautics and Space Administration ;, 1970), by George Kovich and Lewis Research Center (page images at HathiTrust)
• Investigation of injectors for a low-chamber-pressure hydrogen-fluorine rocket engine (National Aeronautics and Space Administration, 1962), by Harold G. Price, Arthur M. Shinn, Robert J. Lubick, and Lewis Research Center (page images at HathiTrust)
• Gaseous-hydrogen, liquid-oxygen rocket combustion at supercritical chamber pressures (National Aeronautics and Space Administration ;, 1967), by Martin Hersch, Edward J. Rice, and Lewis Research Center (page images at HathiTrust)
• Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzles (National Aeronautics and Space Administration, 1960), by Laurence W. Gertsma, Richard A. Yeager, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental performance of liquid hydrogen and liquid fluorine in regeneratively cooled rocket engines (National Aeronautics and Space Administration, 1959), by H. W. Douglass, H. G. Price, G. Hennings, and Langley Research Center (page images at HathiTrust)
• Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid (National Advisory Committee for Aeronautics, 1950), by Gerald Morrell, Jack C. Humphrey, John L. Sloop, Dezso J. Ladanyi, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Chemical and physical factors affecting combustion in fuel : nitric acid systems (National Advisory Committee for Aeronautics, 1958), by James Baker, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• An experimental investigation of the effect of high-pressure tailpipe length on the performance of solid-propellant motors for rocket-powered aircraft (National Advisory Committee for Aeronautics, 1952), by Charles J. Rodriguez, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Studies of the exhaust products from solid propellant rocket motors (Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, 1976), by R Dawbarn, Max Kinslow, United States National Aeronautics and Space Administration, and Arnold Engineering Development Center (page images at HathiTrust)
• Solid rocket motor igniters. (National Aeronautics and Space Administration;, 1971), by Donald H. Barrett (page images at HathiTrust)

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