Livros sobre o tema "Liquid oxygen and methane"
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J, Nowobilski J., e Lewis Research Center, eds. Airborne rotary air separator study: Final report. Tonawanda, NY: Praxair, Inc., 1992.
Encontre o texto completo da fonteMoore, Steve. Liquid oxygen. Newcastle upon Tyne: Echo Room Press, 1998.
Encontre o texto completo da fonteLaw, Susan. Liquid oxygen therapy at home. Montréal, QC: Agence d'évaluation des technologies et des modes d'intervention en santé, 2005.
Encontre o texto completo da fonteZuckerwar, Allan J. Sound speed measurements in liquid oxygen-liquid nitrogen mixtures. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Encontre o texto completo da fonteA, Santavicca Domenic, e United States. National Aeronautics and Space Administration., eds. Laser induced spark ignition of methane-oxygen mixtures. [Washington, D.C.?: National Aeronautics and Space Administration, 1991.
Encontre o texto completo da fonteShapiro, Wilbur. Sealing technology for liquid oxygen (LOX) turbopumps. [Washington, DC: National Aeronautics and Space Administration, 1988.
Encontre o texto completo da fonteE, Edwards, ed. Composition of the vapour and liquid phases of the system methane nitrogen. [Toronto]: University library, pub. by the Librarian, 1996.
Encontre o texto completo da fonteArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. [Washington, D.C.]: NASA, 1990.
Encontre o texto completo da fonteZuckerwar, Allan J. Contamination of liquid oxygen by pressurized gaseous nitrogen. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Tachnical Information Division, 1989.
Encontre o texto completo da fonteArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. [Washington, D.C.]: NASA, 1990.
Encontre o texto completo da fonteGeorge C. Marshall Space Flight Center., ed. Advanced liquid oxygen (LO₂) propellant conditioning concept testing. Marshall Space Flight Center, Ala: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1995.
Encontre o texto completo da fonteGeorge C. Marshall Space Flight Center., ed. Advanced liquid oxygen (LO₂) propellant conditioning concept testing. Marshall Space Flight Center, Ala: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1995.
Encontre o texto completo da fonteJ, Stochl Robert, Sanabria Rafael e United States. National Aeronautics and Space Administration., eds. A review of candidate multilayer insulation systems for potential use on wet-launched LH □tankage for the Space Exploration Initiative lunar missions. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Encontre o texto completo da fonteKumakawa, Akinaga. Hot gas side heat transfer characeristics of LOX/H2 and LOX/HC type propellants. Tokyo, Japan: National Aerospace Laboratory, 1990.
Encontre o texto completo da fonteI, Verkin B., Selover Theodore B. 1931- e Ghojel J. I, eds. Handbook of properties of condensed phases of hydrogen and oxygen. New York: Hemisphere Pub. Corp., 1991.
Encontre o texto completo da fonteShapiro, Wilbur. Advanced helium purge seals for liquid oxygen (LOX) turbopumps. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.
Encontre o texto completo da fonteArmstrong, Elizabeth S. Liquid oxygen cooling of hydrocarbon fueled rocket thrust chambers. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Encontre o texto completo da fonteEberbach, Marcel. Knocking Combustion of Methane-Based and Highly Knock Resistant Liquid Fuels. Wiesbaden: Springer Fachmedien Wiesbaden, 2021. http://dx.doi.org/10.1007/978-3-658-35178-6.
Texto completo da fonteChen, Yen-Sen. Lox manifold tee analysis: Final report. Huntsville, Ala: SECA, Inc., 1990.
Encontre o texto completo da fonteZuckerwar, Allan J. Preliminary study of gaseous nitrogen-liquid oxygen mixing and self-cleaning. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.
Encontre o texto completo da fonteA, Masters Philip, e United States. National Aeronautics and Space Administration., eds. Liquid oxygen cooling of high pressure LOX/hydrocarbon rocket thrust chambers. [Washington, DC]: National Aeronautics and Space Administration, 1987.
Encontre o texto completo da fonteUnited States. National Aeronautics and Space Administration., ed. Carbon monoxide and oxygen combustion experiments: A demonstration of Mars in situ propellants. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Encontre o texto completo da fonteMaria Celeste de Carvalho Serra. Solubilidade de gases em água e em meios de fermentação. Lisboa: Edic̨ões Colibri, 2007.
Encontre o texto completo da fonteOffice, General Accounting. Air Force contracting: Protecting liquid oxygen/nitrogen plants from contamination : report to the Honorable William Dannemeyer, House of Representatives. Washington, D.C: The Office, 1988.
Encontre o texto completo da fonteC, Rousar D., Wong K. Y e Lyndon B. Johnson Space Center., eds. Ignition characterization of LOX/hydrocarbon propellants: Final report. Houston, Tex: The Center, 1985.
Encontre o texto completo da fonteR, Herring J., e Geological Survey (U.S.), eds. Methane, carbon dioxide, oxygen, and nitrogen in soil gas overlying coal beds of the Upper Cretaceous Fruitland Formation in the San Juan Basin, La Plata County, southwestern Colorado. [Denver, Colo.?]: U.S. Dept. of the Interior, U.S. Geological Survey, 1994.
Encontre o texto completo da fonteCurt, Bilby, e Lewis Research Center, eds. A superconducing quenchgun for delivering lunar derived oxygen to lunar orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1990.
Encontre o texto completo da fonteCurt, Bilby, e Lewis Research Center, eds. A superconducing quenchgun for delivering lunar derived oxygen to lunar orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1990.
Encontre o texto completo da fonteArmstrong, Elizabeth S. Test program to provide confidence in liquid oxygen cooling of hydrocarbon fueled rocket thrust chambers. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Encontre o texto completo da fonteV, Shebalin John, e Langley Research Center, eds. Support of the eight-foot high-temperature tunnel modifications project: Final report for the period May 16, 1985 to May 15, 1986. Norfolk, Va: Old Dominion University Research Foundation, 1987.
Encontre o texto completo da fonteV, Shebalin John, e Langley Research Center, eds. Support of the eight-foot high-temperature tunnel modifications project: Final report for the period May 16, 1985 to May 15, 1986. Norfolk, Va: Old Dominion University Research Foundation, 1987.
Encontre o texto completo da fonteS, Armstrong Elizabeth, Price Harold G e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. [Washington, DC]: National Aeronautics and Spac14., 1988.
Encontre o texto completo da fonteRivers, H. Kevin. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Encontre o texto completo da fonteCenter, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Encontre o texto completo da fonteCenter, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Encontre o texto completo da fonteMasters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Cleveland, Ohio: Lewis Research Center, 1988.
Encontre o texto completo da fonteS, Armstrong Elizabeth, Price Harold G e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. [Washington, DC]: National Aeronautics and Spac14., 1988.
Encontre o texto completo da fonteMorris, Michelle L. Evaluation of alternatives for trichlorotrifluoroethane (CFC-113) to clean and verify liquid oxygen system. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Encontre o texto completo da fonteCenter, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Encontre o texto completo da fonteAl-Harbi, Ahmed Baker. Synthesis and Coordination Chemistry of Oxygen Rich Ligands: Bis(oxoimidazolyl)hydroborato, Tris(oxoimidazolyl)hydroborato and Tris(2-pyridonyl)methane. [New York, N.Y.?]: [publisher not identified], 2014.
Encontre o texto completo da fonteTimothy, Martin, Hodgson Ed e United States. National Aeronautics and Space Administration., eds. Extended mobility unit subcritical liquid oxygen storage and supply system (EMU SLOSSS): Conceptual design study report. Denver, Colo: Martin Marietta, Civil Space and Communications Company, 1992.
Encontre o texto completo da fonteW, Lariviere Brian, e Lewis Research Center, eds. Test results of the RS-44 integrated component evaluator liquid oxygen-hydrogen rocket engine: Final report. Cleveland, Ohio: NASA-Lewis Research Center, 1993.
Encontre o texto completo da fonteW, Lariviere B., e Lewis Research Center, eds. Test results of the RS-44 integrated component evaluator liquid oxygen-hydrogen rocket engine: Final report. Cleveland, Ohio: NASA-Lewis Research Center, 1993.
Encontre o texto completo da fonteOffice, General Accounting. Air Force contracting: Protecting liquid oxygen/nitrogen plants from contamination : report to the Honorable William Dannemeyer, House of Representatives. Washington, D.C: The Office, 1988.
Encontre o texto completo da fonteAnderson, John. Conceptual design study report: Extended Mobility Unit Subcritical Liquid Oxygen Storage and Supply System (EMU SLOSSS) : contract NAS9-18608. Denver, Colo: Martin Marietta, Civil Space and Communications Company, 1992.
Encontre o texto completo da fonteUnited States. National Aeronautics and Space Administration., ed. Final report on the development of methodologies and solvent systems to replace CFC-113 in the validation of large-scale spacecraft hardware: NASA research grant award no. NAG10-0169. [Washington, DC: National Aeronautics and Space Administration, 1996.
Encontre o texto completo da fonteA, Dudzinski Leonard, e NASA Glenn Research Center, eds. "2001, a Space Odyssey" revisited: The feasibility of 24 hour commuter flights to the Moon using NTR propulsion with LUNOX afterburners. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Encontre o texto completo da fonteS, Zakany James, e United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Encontre o texto completo da fonteGeorge C. Marshall Space Flight Center., ed. STS propellant densification feasibility study data book. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994.
Encontre o texto completo da fonteUnited States. National Aeronautics and Space Administration., ed. Development of nonintrusive, scatter-independent techniques for measurement of liquid density inside dense sprays: Interim report. [Washington, DC: National Aeronautics and Space Administration, 1994.
Encontre o texto completo da fonte