Books on the topic 'Liquid system'

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

E, Fradkov V., and United States. National Aeronautics and Space Administration., eds. 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., and United States. National Aeronautics and Space Administration., eds. Large liquid rocket engine transient performance simulation system. West Palm Beach, FL: Pratt & Whitney, 1989.

D, Southwick R., and United States. National Aeronautics and Space Administration., eds. 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., ed. 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, ed. 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., ed. 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., ed. 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., ed. 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., ed. 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., ed. 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., ed. 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., ed. 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., ed. 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), ed. 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., ed. 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., ed. 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., and George C. Marshall Space Flight Center., eds. 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, and United States. Environmental Protection Agency. Control Technology Center, eds. 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, and Lewis Research Center, eds. 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., ed. 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, and Air and Energy Engineering Research Laboratory, eds. 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, ed. 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., 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.

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., ed. 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, and National Research Council (U.S.). Division on Engineering and Physical Sciences, eds. 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, and United States. National Aeronautics and Space Administration., eds. 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., ed. 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., ed. 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, and 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.

United States. National Aeronautics and Space Administration., ed. 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., ed. 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, ed. 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.