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Results 1 to 25 of 268

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Characteristics, supply and use of the hydrofluorocarbons HFA 227 and HFA 134a for medical aerosols in the past, present and future. Manufacturers perspectivesPISCHTIAK, Anja H.Chimica oggi. 2002, Vol 20, Num 3-4, pp 14-19, issn 0392-839X, 5 p.Article

AEROSOL-TREIBMITTEL = LES PROPULSEURS POUR AEROSOLSKUBLER H.1980; AEROSOL REP.; DEU; DA. 1980; VOL. 19; NO 5; PP. 149-154; (2 P.); IDEM ENG FREArticle

Il razzo a liquido = Liquid fuel rocketCAPUTO DI CALVISI, Carmelo.Termotecnica (Milano). 2003, Vol 57, Num 5, pp 53-54, issn 0040-3725, 2 p.Article

Adiabatic calorimetry for evaluation of thermally induced reactions in liquid propellantsKLEIN, N; LEVERITT, C. S.Thermochimica acta. 1990, Vol 166, pp 231-239, issn 0040-6031, 9 p.Conference Paper

Degradation of explosive propellants by in-vessel compostingBROWN, K. W; THOMAS, J. C; SEAGO, O. J et al.Biocycle. 1995, Vol 36, Num 9, pp 56-58, issn 0276-5055Article

Analysis of flame patterns in cryogenic propellant combustionSNYDER, R; HERDING, G; ROLON, J. C et al.Combustion science and technology. 1997, Vol 124, Num 1-6, pp 331-370, issn 0010-2202Article

Analysis of deflagration to detonation transition in high-energy solid propellantsBUTLER, P. B; KRIER, H.Combustion and flame. 1986, Vol 63, Num 1-2, pp 31-48, issn 0010-2180Article

Plasma ignition of liquid propellantCATTOLICA, R. J; KLEIN, N.Combustion science and technology. 1987, Vol 56, Num 4-6, pp 139-148, issn 0010-2202Article

Design, fabrication and thrust measurement of a micro liquid monopropellant thrusterJEONGMOO HUH; SEJIN KWON.Journal of micromechanics and microengineering (Print). 2014, Vol 24, Num 10, issn 0960-1317, 104001.1-104001.9Conference Paper

Supercritical Heat Transfer of Cryogenic-Propellant Methane in Rectangular Engine Cooling ChannelsBO RUAN; HUA MENG.Journal of thermophysics and heat transfer. 2012, Vol 26, Num 2, pp 313-321, issn 0887-8722, 9 p.Article

High-Resolution Numerical Method for Supercritical Flows with Large Density VariationsTERASHIMA, Hiroshi; KAWAI, Soshi; YAMANISHI, Nobuhiro et al.AIAA journal. 2011, Vol 49, Num 12, pp 2658-2672, issn 0001-1452, 15 p.Article

Condensed phase decomposition and gas phase combustion of hydrazinium nitroformateDRAGOMIR, O. E; TUMMERS, M. J; VAN VEEN, E. H et al.Combustion and flame. 2009, Vol 156, Num 9, pp 1810-1817, issn 0010-2180, 8 p.Article

Propellant preservation using re-liquefiersKITTEL, Peter.Cryogenics (Guildford). 2001, Vol 41, Num 11-12, pp 841-844, issn 0011-2275Conference Paper

The Lewis number under supercritical conditionsHARSTAD, K; BELLAN, J.International journal of heat and mass transfer. 1999, Vol 42, Num 6, pp 961-970, issn 0017-9310Article

Liquid hydrogen densification heat exchangerMCINTOSH, G. E; STOCHL, R. J; TOMSIK, T. M et al.Advances in cryogenic engineering. 1998, Vol 43, pp 1009-1016, issn 0065-2482, AConference Paper

Vélocimétrie par suivi de particules dans un brouillard d'oxygène liquide en combustion = Particle velocimetry of combustion of liquid oxygen sprayLECOURT, R; OSCHWALD, M.Visualisation et traitement d'images en mécanique des fluides. Colloque nationalVISU 97. 1997, pp 113-118, isbn 2-87717-061-6Conference Paper

Continuing patient care with metered-dose inhalersWOODCOCK, A.Journal of aerosol medicine. 1995, Vol 8, pp S5-S10, issn 0894-2684, SUP2Conference Paper

Impinging jet atomization at elevated and supercritical ambient temperature and pressure conditionsSHEN, Y. B; POULIKAKOS, D.Experimental heat transfer. 1998, Vol 11, Num 1, pp 23-40, issn 0891-6152Article

Development of propulsion system for ISAS lunar exploration projectONO, A; NOGAWA, K; IIHARA, S et al.Ishikawajima-Harima Giho. 1995, Vol 35, Num 2, pp 77-82, issn 0578-7904Article

Simulation of composite propellant agingKHAN, M. B.Polymer-plastics technology and engineering (Softcover ed). 1993, Vol 32, Num 5, pp 467-489, issn 0360-2559Article

Uniaxial compression testing of M30 and JA2 gun propellants using a statistical design strategyGAZONAS, G. A; FORD, J. C.Experimental mechanics. 1992, Vol 32, Num 2, pp 154-162, issn 0014-4851Article

Computer simulation of a test rig to model sloshing in spin-stabilized satellitesFLUGRAD, D. R; OBERMAIER, L. A.Journal of dynamic systems, measurement, and control. 1992, Vol 114, Num 4, pp 689-698, issn 0022-0434Article

Aerosol propellant interference with clinical mass spectrometersKHARASCH, E. D; SIVARAJAN, M.Journal of clinical monitoring. 1991, Vol 7, Num 2, pp 172-174, issn 0748-1977, 3 p.Article

The interaction of flammability and toxicity in an aerosol productMOOZ, W. E.Journal of hazardous materials. 1985, Vol 10, Num 2-3, pp 179-187, issn 0304-3894Article

The effect of reduction of propellant mass fraction on the injection profile of metered dose inhalersDEHAO JU; SHRIMPTON, John; HEARN, Alex et al.International journal of pharmaceutics (Print). 2010, Vol 391, Num 1-2, pp 221-229, issn 0378-5173, 9 p.Article

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