Books on the topic 'Pressure chamber'

George C. Marshall Space Flight Center., ed. Pressure fed thrust chamber technology: Test plan. Sacramento, Calif: Aerojet Propulsion Division, 1990.

Schins, H. Shock tubes: Compressions in the low pressure chamber. Luxembourg: Commission of the European Communities, 1986.

United States. National Aeronautics and Space Administration., ed. Stigmatically focusing partial pressure analyzer with dual chamber ion source. Washington, DC: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration., ed. Pressure fed thrust chamber technology program: Contract NAS 8-37365, final report. [Washington, DC: National Aeronautics and Space Administration, 1992.

Laura, Salamacha, and Ames Research Center, eds. Lower body negative pressure chamber: Design and specifications for tilt-table mounting. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

Jankovsky, Robert S. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Kumakawa, Akinaga. Characteristics of heat transfer to nickel plated chamber walls of high pressure rocket combustors. Tokyo: National Aerospace Laboratory, 1991.

Masters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Cleveland, Ohio: Lewis Research Center, 1988.

M, Kazaroff John, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Jankowsky, Robert S. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. [Cleveland, Ohio]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

M, Kazaroff John, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

M, Kazaroff John, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

S, Armstrong Elizabeth, Price Harold G, and 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.

S, Armstrong Elizabeth, Price Harold G, and 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.

Rosindale, Ian J. Modelling the thermal behaviour of the metal injection system in the hot chamber pressure die casting process. Manchester: UMIST, 1997.

Standards, Association of Australia Committee BD/42 Methods of Testing Concrete. Methods of testing concrete: Determination of air content of freshly mixed concrete - measuring reduction in air pressure in chamber above concrete. [North Sydney, N.S.W.]: Standards Australia, 1999.

J, Pavli Albert, Kacynski Kenneth J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m℗ø(350 psia). [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Smith, Tamara A. Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia). Cleveland, Ohio: Lewis Research Center, 1987.

Stahl, Bernhard. Messung von Druckschwankungen in einer Resonanzkammer mit laserinduzierter Jod-Fluoreszenz. Koln: DFVLR, 1987.

Center, Langley Research, ed. Cryogenic pressure calibrator for wide temperature electronically scanned (ESP) pressure modules. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

United States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

A, Masters Philip, and 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.

United States. National Aeronautics and Space Administration., ed. Construction of a direct water-injected two-stroke engine for phased direct fuel injection-high pressure charging investigations: Order number, A49222D (LAS), April 1, 1998. Tecumseh, MI: Orbital Engine Company (USA) Inc., 1998.

United States. National Aeronautics and Space Administration., ed. SiC recession due to SiO₂ scale volatility under combustor conditions. Brook Park, Ohio: NYMA, Inc., 1997.

United States. National Aeronautics and Space Administration., ed. SiC recession due to SiO₂ scale volatility under combustor conditions. Brook Park, Ohio: NYMA, Inc., 1997.

A, Knight B., Shirley J. A, and Lewis Research Center, eds. Development of UV optical measurements of nitric oxide and hydroxyl radical at the exit of high pressure gas turbine combustors: Final report (March 1995 to March 1998). [East Hartford, CT]: United Technologies Research Center, 1998.

Felton, William B. Observations soumises à la considération des membres de la Législature et du public en général sur un rapport d'un comité de la Chambre d'assemblée. [S.l: s.n., 1985.

Hamed, A. Flow characteristics in boundary layer bleed slots with plenum. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Hamed, A. Flow characteristics in boundary layer bleed slots with plenum. [Washington, D.C: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. In situ detection of tropospheric OH, HO,́ NO,́ and NO by laser-induced fluorescence in detection chambers at reduced pressures: For the period, 1 October, 1991 to 30 April, 1992. University Park, PA: Dept. of Meteorology, Pennsylvania State University, 1992.

Canadian Study of Parliament Group. Seminars on confidence: The British House of Commons and the Ontario Legislature and Lobbying : will registration of lobbyists work?: Ottawa, 20-21 March 1986 = Colloques sur la confiance : la Chambre des communes britannique et l'Assemblée législative de l'Ontario et les groupes de pression : l'enregistrement des groupes de pression peut-il fonctionner? : Ottawa, 20-21 mars 1986. Ottawa: Canadian Study of Parliament Group, 1986.

Prognoz termomekhanicheskogo sostoinia mnogoletnemerzlogo massiva. Yakutsk: YaNTs SO AN SSSR, 1989.

United States. National Aeronautics and Space Administration., ed. In situ detection of tropospheric OH, HO,́ NO,́ and NO by laser-induced fluorescence in detection chambers at reduced pressures: Final report for NASA grant NAG-1-1057 for the period, 1 October, 1989 to 31 March, 1993. University Park, PA: Dept. of Meteorology, Pennsylvania State University, 1992.

Pressure Chamber. Legend Press, 2021.

National Aeronautics and Space Administration (NASA) Staff. Pressure Fed Thrust Chamber Technology Program. Independently Published, 2018.

Hezroni, Nir. Pressure Chamber: A Gripping Thriller Set in Tel Aviv. Legend Press, 2021.

Pressure fed thrust chamber technology program: Contract number NAS8-37365 final report. Sacramento, Calif: Aerojet Propulsion Division, 1992.

High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

National Aeronautics and Space Administration (NASA) Staff. High-Area-Ratio Rocket Nozzle at High Combustion Chamber Pressure: Experimental and Analytical Validation. Independently Published, 2018.

Plume diagnostics of the RSRM static firings for the pressure perturbation studies. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Boundary layer development as a function of chamber pressure in the NASA Lewis 1030:1 area ratio rocket nozzle. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.

A performance comparison of two small rocket nozzles. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Schairer, John R., and Steven J. Keteyian. Pathophysiology and causes of pericardial tamponade. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780199600830.003.0166.

Hunter, Nicole. Emotional Coloring Book: Over 45+ Coal Chamber Inspired Designs That Will Lower You Fatigue, Blood Pressure and Reduce Activity of Stress Hormones. Independently Published, 2021.

Gorenek, Bulent. Temporary pacing. Oxford University Press, 2015. http://dx.doi.org/10.1093/med/9780199687039.003.0026.

Gorenek, Bulent. Temporary pacing. Oxford University Press, 2018. http://dx.doi.org/10.1093/med/9780199687039.003.0026_update_001.