Książki na temat „Liquid oxygen and methane”
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J, Nowobilski J., i Lewis Research Center, red. Airborne rotary air separator study: Final report. Tonawanda, NY: Praxair, Inc., 1992.
Znajdź pełny tekst źródłaMoore, Steve. Liquid oxygen. Newcastle upon Tyne: Echo Room Press, 1998.
Znajdź pełny tekst źródłaLaw, Susan. Liquid oxygen therapy at home. Montréal, QC: Agence d'évaluation des technologies et des modes d'intervention en santé, 2005.
Znajdź pełny tekst źródłaZuckerwar, 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.
Znajdź pełny tekst źródłaA, Santavicca Domenic, i United States. National Aeronautics and Space Administration., red. Laser induced spark ignition of methane-oxygen mixtures. [Washington, D.C.?: National Aeronautics and Space Administration, 1991.
Znajdź pełny tekst źródłaShapiro, Wilbur. Sealing technology for liquid oxygen (LOX) turbopumps. [Washington, DC: National Aeronautics and Space Administration, 1988.
Znajdź pełny tekst źródłaE, Edwards, red. Composition of the vapour and liquid phases of the system methane nitrogen. [Toronto]: University library, pub. by the Librarian, 1996.
Znajdź pełny tekst źródłaArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. [Washington, D.C.]: NASA, 1990.
Znajdź pełny tekst źródłaZuckerwar, 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.
Znajdź pełny tekst źródłaArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. [Washington, D.C.]: NASA, 1990.
Znajdź pełny tekst źródłaGeorge C. Marshall Space Flight Center., red. 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.
Znajdź pełny tekst źródłaGeorge C. Marshall Space Flight Center., red. 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.
Znajdź pełny tekst źródłaJ, Stochl Robert, Sanabria Rafael i United States. National Aeronautics and Space Administration., red. 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.
Znajdź pełny tekst źródłaKumakawa, Akinaga. Hot gas side heat transfer characeristics of LOX/H2 and LOX/HC type propellants. Tokyo, Japan: National Aerospace Laboratory, 1990.
Znajdź pełny tekst źródłaI, Verkin B., Selover Theodore B. 1931- i Ghojel J. I, red. Handbook of properties of condensed phases of hydrogen and oxygen. New York: Hemisphere Pub. Corp., 1991.
Znajdź pełny tekst źródłaShapiro, Wilbur. Advanced helium purge seals for liquid oxygen (LOX) turbopumps. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.
Znajdź pełny tekst źródłaArmstrong, Elizabeth S. Liquid oxygen cooling of hydrocarbon fueled rocket thrust chambers. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Znajdź pełny tekst źródłaEberbach, 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.
Pełny tekst źródłaChen, Yen-Sen. Lox manifold tee analysis: Final report. Huntsville, Ala: SECA, Inc., 1990.
Znajdź pełny tekst źródłaZuckerwar, Allan J. Preliminary study of gaseous nitrogen-liquid oxygen mixing and self-cleaning. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.
Znajdź pełny tekst źródłaA, Masters Philip, i United States. National Aeronautics and Space Administration., red. Liquid oxygen cooling of high pressure LOX/hydrocarbon rocket thrust chambers. [Washington, DC]: National Aeronautics and Space Administration, 1987.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Carbon monoxide and oxygen combustion experiments: A demonstration of Mars in situ propellants. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Znajdź pełny tekst źródłaMaria Celeste de Carvalho Serra. Solubilidade de gases em água e em meios de fermentação. Lisboa: Edic̨ões Colibri, 2007.
Znajdź pełny tekst źródłaOffice, 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.
Znajdź pełny tekst źródłaC, Rousar D., Wong K. Y i Lyndon B. Johnson Space Center., red. Ignition characterization of LOX/hydrocarbon propellants: Final report. Houston, Tex: The Center, 1985.
Znajdź pełny tekst źródłaR, Herring J., i Geological Survey (U.S.), red. 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.
Znajdź pełny tekst źródłaCurt, Bilby, i Lewis Research Center, red. A superconducing quenchgun for delivering lunar derived oxygen to lunar orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1990.
Znajdź pełny tekst źródłaCurt, Bilby, i Lewis Research Center, red. A superconducing quenchgun for delivering lunar derived oxygen to lunar orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1990.
Znajdź pełny tekst źródłaArmstrong, 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.
Znajdź pełny tekst źródłaV, Shebalin John, i Langley Research Center, red. 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.
Znajdź pełny tekst źródłaV, Shebalin John, i Langley Research Center, red. 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.
Znajdź pełny tekst źródłaS, Armstrong Elizabeth, Price Harold G i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. [Washington, DC]: National Aeronautics and Spac14., 1988.
Znajdź pełny tekst źródłaRivers, 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.
Znajdź pełny tekst źródłaCenter, Langley Research, red. 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.
Znajdź pełny tekst źródłaCenter, Langley Research, red. 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.
Znajdź pełny tekst źródłaMasters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Cleveland, Ohio: Lewis Research Center, 1988.
Znajdź pełny tekst źródłaS, Armstrong Elizabeth, Price Harold G i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. [Washington, DC]: National Aeronautics and Spac14., 1988.
Znajdź pełny tekst źródłaMorris, 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.
Znajdź pełny tekst źródłaCenter, Langley Research, red. 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.
Znajdź pełny tekst źródłaAl-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.
Znajdź pełny tekst źródłaTimothy, Martin, Hodgson Ed i United States. National Aeronautics and Space Administration., red. 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.
Znajdź pełny tekst źródłaW, Lariviere Brian, i Lewis Research Center, red. Test results of the RS-44 integrated component evaluator liquid oxygen-hydrogen rocket engine: Final report. Cleveland, Ohio: NASA-Lewis Research Center, 1993.
Znajdź pełny tekst źródłaW, Lariviere B., i Lewis Research Center, red. Test results of the RS-44 integrated component evaluator liquid oxygen-hydrogen rocket engine: Final report. Cleveland, Ohio: NASA-Lewis Research Center, 1993.
Znajdź pełny tekst źródłaOffice, 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.
Znajdź pełny tekst źródłaAnderson, 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.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. 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.
Znajdź pełny tekst źródłaA, Dudzinski Leonard, i NASA Glenn Research Center, red. "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.
Znajdź pełny tekst źródłaS, Zakany James, i United States. National Aeronautics and Space Administration., red. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Znajdź pełny tekst źródłaGeorge C. Marshall Space Flight Center., red. STS propellant densification feasibility study data book. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Development of nonintrusive, scatter-independent techniques for measurement of liquid density inside dense sprays: Interim report. [Washington, DC: National Aeronautics and Space Administration, 1994.
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