Książki na temat „Liquid system”

United States. National Aeronautics and Space Administration., red. Kinetics of diffusional droplet growth in a liquid/liquid two-phase system. [Washington, DC: National Aeronautics and Space Administration, 1992.

E, Fradkov V., i United States. National Aeronautics and Space Administration., red. Kinetics of diffusional droplet growth in a liquid-liquid two-phase system: Final technical report. [Washington, DC: National Aeronautics and Space Administration, 1995.

Trindade, Sergio C. Oxygenated transport liquid fuels: The total system = Combustibles liquides oxigenes pour le transport : le systeme globale. London: World Energy Conference, 1989.

D, Southwick R., i United States. National Aeronautics and Space Administration., red. Large liquid rocket engine transient performance simulation system. West Palm Beach, FL: Pratt & Whitney, 1989.

D, Southwick R., i United States. National Aeronautics and Space Administration., red. Large liquid rocket engine transient performance simulation system. West Palm Beach, Fl: United Technologies, Pratt & Whitney ; [Washington, DC, 1989.

United States. National Aeronautics and Space Administration., red. Kinetics of diffusional droplet growth in a liquid/liquid two-phase system: Final report. [Washington, DC: National Aeronautics and Space Administration, 1993.

Center, Lewis Research, red. Fatigue criterion to system design, life and reliabilty. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

George C. Marshall Space Flight Center., red. Liquid Rocket Booster (LRB) for the Space Transportation System (STS) systems study. [New Orleans, La.]: Martin Marietta Manned Space Systems, 1990.

United States. National Aeronautics and Space Administration., red. Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study. [New Orleans, La.]: Martin Marietta, Manned Space Systems, 1989.

United States. National Aeronautics and Space Administration., red. Liquid rocket booster (LRB) for the Space Transportation System (STS) Systems Study. [New Orleans, La.?]: Martin Marietta, Manned Space Systems, 1989.

United States. National Aeronautics and Space Administration., red. Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study. [New Orleans, La.?]: Martin Marietta, Manned Space Systems, 1989.

United States. National Aeronautics and Space Administration., red. Liquid Rocket Booster (LRB) for the Space Transportation System (STS) systems study. [Washington, DC: National Aeronautics and Space Administration, 1990.

United States. National Aeronautics and Space Administration., red. Liquid Rocket Booster (LAB) for the Space Transportation System (STS) Systems Study. [New Orleans, La.]: Martin Marietta, Manned Space Systems, 1989.

United States. National Aeronautics and Space Administration., red. Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study. [New Orleans, La.?]: Martin Marietta, Manned Space Systems, 1989.

United States. National Aeronautics and Space Administration., red. Liquid Rocket Booster (LRB) for the Space Transportation System (STS) systems study. [Washington, DC: National Aeronautics and Space Administration, 1990.

Michoud Assembly Facility (George C. Marshall Space Flight Center), red. Liquid Rocket Booster (LRB) for the Space Transportation System (STS) systems study. [New Orleans, La.]: Martin Marietta, Manned Space Systems, 1991.

United States. National Aeronautics and Space Administration., red. Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study. [New Orleans, La.?]: Martin Marietta, Manned Space Systems, 1989.

United States. National Aeronautics and Space Administration., red. Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study. [New Orleans, La.]: Martin Marietta, Manned Space Systems, 1989.

Theofanous, T. G. Performance of the liquid reactivity control system in BWRs. Washington, DC: Division of Regulatory Applications, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1989.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion instabilities in liquid-fuelled propulsion systems. Neuilly sur Seine, France: AGARD, 1989.

D, Southwick R., i George C. Marshall Space Flight Center., red. Large liquid rocket engine transient performance simulation system: Final report. West Palm Beach, FL: United Technologies Corporation, Pratt & Whitney, Government Engine Business, 1991.

Randy, Merritt, Williamson Ashley D i United States. Environmental Protection Agency. Control Technology Center, red. Evaluation of a liquid chemical scrubber system for styrene removal. Research Triangle Park, NC: U.S. Environmental Protection Agency, Control Technology Center, 1994.

Chau, Kwok Wing. Knowledge-based system for analysis and design of liquid retaining structures. Hauppauge, N.Y: Nova Science, 2011.

Ronald, De Hoff, i Lewis Research Center, red. Development of life prediction capabilities for liquid propellant rocket engines: Diagnostic system architecture study : final report. Sacramento, Calif: GenCorp, Aerojet Propulsion Division, 1991.

Office, General Accounting. Army armored systems: Advanced Field Artillery System experiences problems with liquid propellant : report to selected members of Congress. Washington, D.C: The Office, 1994.

Joint Panel on Oceanographic Tables and Standards. Carbon Dioxide Sub-Group., red. Thermodynamics of the carbon dioxide system in seawater: Report. Paris: Unesco, 1987.

Marriott, R. An acoustic resonance spectroscopy system for the assessment of liquid-filled cylinders. Manchester: UMIST, 1993.

Randy, Merritt, Williamson Ashley D i Air and Energy Engineering Research Laboratory, red. Evaluation of a liquid chemical scrubber system for styrene removal: Project summary. Research Triangle Park, NC: U.S. Environmental Protection Agency, Air and Energy Engineering Research Laboratory, 1995.

E, Edwards, red. Composition of the vapour and liquid phases of the system methane nitrogen. [Toronto]: University library, pub. by the Librarian, 1996.

George 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.

Lloyd, Jason Michael. A feasibility study of liquid phase siinter forming of a model ceramic system. Monterey, Calif: Naval Postgraduate School, 1998.

Limited, Hitachi. Hitachi microcomputer system liquid crystal display timing controller (LCTC) HD63645F/HD64645F user's manual. Tokyo: Hitachi Ltd, 1987.

United 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.

French, J. B. Liquid sample introduction system (LIQSI): Final report URIF Grant no. TO-5-014 in cooperation with SCIEX Division of MDS Health Group Limited, July 1, 1987 - June 30, 1987. [Toronto, Ont.]: University of Toronto, Institute for Aerospace Studies, 1989.

National Research Council (U.S.). Committee on Review and Evaluation of the Army Non-Stockpile Chemical Materiel Disposal Program, National Research Council (U.S.). Board on Army Science and Technology i National Research Council (U.S.). Division on Engineering and Physical Sciences, red. Evaluation of alternative technologies for disposal of liquid wastes from the explosive destruction system. Washington, D.C: National Academy Press, 2001.

Morris, 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.

R, Balasubramaniam, i United States. National Aeronautics and Space Administration., red. Thermocapillary migration of liquid droplets in a temperature gradient in a density matched system. [Washington, DC]: National Aeronautics and Space Administration, 1990.

United States. National Aeronautics and Space Administration., red. Performance tests of a liquid hydrogen propellant densification ground system for the X33/RLV. [Washington, DC]: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., red. Developments in REDES: The rocket engine design expert system. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Faghri, Amir. Numerical and experimental analysis of a thin liquid film on a rotating disk related to development of a spacecraft absorption cooling system. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Lin, Chin-Shun. Vapor condensation on liquid surface due to laminar jet-induced mixing: The effects of system parameters. [Washington, D.C.]: NASA, 1990.

Timothy, 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.

United States. National Aeronautics and Space Administration., red. Trade study plan for reusable hydrogen composite tank system (RHCTS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.

United States. National Aeronautics and Space Administration., red. Zero-G Thermodynamic Venting System (TVS) performance prediction program. Downey, Calif: Rockwell Aerospace, 1994.

Anderson, 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.

1900-, Keenan Joseph Henry, red. Steam tables: Thermodynamic properties of water including vapor, liquid, and solid phases (International system of units--S.I.). Malabar, Fla: Krieger Pub. Co., 1992.

Liquid Biphasic System. Elsevier, 2021. http://dx.doi.org/10.1016/c2019-0-01128-4.

National Aeronautics and Space Administration (NASA) Staff. Kinetics of Diffusional Droplet Growth in a Liquid/Liquid Two-Phase System. Independently Published, 2018.

National Aeronautics and Space Administration (NASA) Staff. Kinetics of Diffusional Droplet Growth in a Liquid/Liquid Two-Phase System. Independently Published, 2018.

Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study. [New Orleans, La.]: Martin Marietta, Manned Space Systems, 1989.