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Results 1 to 25 of 148

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Steady-state high pressure LOx/H2 rocket engine combustionSMITH, Joshua J; SCHNEIDER, Gerald; SUSLOV, Dmitry et al.Aerospace science and technology. 2007, Vol 11, Num 1, pp 39-47, issn 1270-9638, 9 p.Conference Paper

Design analysis of Rayleigh-step floating-ring sealsARTILES, A; SHAPIRO, W; JONES, H. F et al.ASLE transactions. 1984, Vol 27, Num 4, pp 321-331, issn 0569-8197Article

Two-phase flow characteristics of liquid oxygen flow in low pressure liquid rocket engineCHO, Namkyung; KIM, Seunghan; KIM, Youngmog et al.Cryogenics (Guildford). 2004, Vol 44, Num 6-8, pp 493-500, issn 0011-2275, 8 p.Conference Paper

Dielectric coefficient and density of subcooled liquid oxygenCELIK, D; VAN SCIVER, S. W.Cryogenics (Guildford). 2005, Vol 45, Num 5, pp 356-361, issn 0011-2275, 6 p.Article

Numerical analysis of regenerative cooling in liquid propellant rocket enginesULAS, A; BOYSAN, E.Aerospace science and technology (Imprimé). 2013, Vol 24, Num 1, pp 187-197, issn 1270-9638, 11 p.Article

Liquid oxygen liquid acquisition device bubble point tests with high pressure lox at elevated temperaturesJURNS, J. M; HARTWIG, J. W.Cryogenics (Guildford). 2012, Vol 52, Num 4-6, pp 283-289, issn 0011-2275, 7 p.Conference Paper

The role of flight experiments in the development of cryogenic fluid management technologiesCHATO, David J.Cryogenics (Guildford). 2006, Vol 46, Num 2-3, pp 82-88, issn 0011-2275, 7 p.Conference Paper

Investigation of helium injection cooling to liquid oxygen under pressurized conditionCHO, Namkyung; KWON, Ohsung; KIM, Youngmog et al.Cryogenics (Guildford). 2006, Vol 46, Num 11, pp 778-793, issn 0011-2275, 16 p.Article

Substitute mixtures for LOX droplet vaporization studyNICOLI, C; HALDENWANG, P; DAOU, J et al.Combustion science and technology. 1996, Vol 112, pp 55-74, issn 0010-2202Article

A new portable oxygen system using liquid oxygenRAMAGE, C. M. H; KEE, S. S; BRISTOW, A et al.Anaesthesia. 1991, Vol 46, Num 5, pp 395-397, issn 0003-2409, 3 p.Article

A system for cooling liquid oxygen to 58 KANDREEV, G. A.Chemical and petroleum engineering. 1999, Vol 35, Num 9-10, pp 535-538, issn 0009-2355Article

P8 : The new French/German test facility for H2/O2 high pressure rocket engine combustion researchKOSCHEL, W. W; HAIDN, O. J.International journal of hydrogen energy. 1998, Vol 23, Num 8, pp 683-694, issn 0360-3199, 11 p.Article

Liquid oxygen systems in emergency care vehiclesHAYES, J.Urgences médicales (Paris). 1990, Vol 9, Num 3, pp 174-177, issn 0923-2524, 4 p.Conference Paper

Oxygène liquide dans une ambulance SMUR. Essai préliminaire = Liquid oxygene in medical emergency ambulanceGABE, J. L; METADIER, D; MARCHADIER, C et al.Urgences médicales (Paris). 1990, Vol 9, Num 3, pp 178-181, issn 0923-2524, 4 p.Conference Paper

Conditions d'emploi de l'oxygène liquide = Use conditions for liquid oxygenBRUEL, J.Urgences médicales (Paris). 1990, Vol 9, Num 3, pp 168-171, issn 0923-2524, 4 p.Article

Etude expérimentale du mécanisme de développement et de séparation de bulles de gaz en conditions d'atténuation de gravitationGLADCHENKO, G. M; KIRICHENKO, YU. A; RUSANOV, K. V et al.Inženerno-fizičeskij žurnal. 1990, Vol 58, Num 2, pp 190-196, issn 0021-0285, 7 p.Article

Numerical simulation of droplet vaporization and ignition with detailed chemistryRIEDEL, U; WARNATZ, J; AOUINA, Y et al.VDI-Berichte. 1997, pp 419-424, issn 0083-5560, isbn 3-18-091313-4Conference Paper

Surchauffes limites de l'oxygène liquide dans des cellules métalliquesKAVERIN, A. M; BAJDAKOV, V. G; SKRIPOV, V. P et al.Žurnal tehničeskoj fiziki. 1985, Vol 55, Num 6, pp 1220-1222, issn 0044-4642Article

Analysis of spiral-groove face seals for liquid oxygenSHAPIRO, W; WACOWIT, J; JONES, H. F et al.ASLE transactions. 1984, Vol 27, Num 3, pp 177-188, issn 0569-8197Article

A review of experimental methods for solid solubility determination in cryogenic systemsDE STEFANI, V; BABA-AHMED, A; RICHON, D et al.Cryogenics (Guildford). 2004, Vol 44, Num 9, pp 631-641, issn 0011-2275, 11 p.Article

Simple and inexpensive technique for measuring the transition temperature of superconducting thick films from 60 to 300 K using liquid nitrogen and subcooled liquid oxygenMOUSSA, M. A. A.Cryogenics (Guildford). 2009, Vol 49, Num 1, pp 17-20, issn 0011-2275, 4 p.Article

Foam insulation for a liquid oxygen densifierMCINTOSH, G. E; STUCKENSCHMIDT, R.Cryogenics (Guildford). 2012, Vol 52, Num 4-6, pp 248-250, issn 0011-2275, 3 p.Conference Paper

Surface Tension of Liquid Iron as Functions of Oxygen Activity and TemperatureMOROHOSHI, Keisuke; UCHIKOSHI, Masahito; ISSHIKI, Minoru et al.ISIJ international. 2011, Vol 51, Num 10, pp 1580-1586, issn 0915-1559, 7 p.Article

Structure et stabilisation des flammes cryotechniques = Structure and Stabilization of Cryogenic Spray FlamesJuniper, Matthew; Candel, Sébastien.2001, 248 p.Thesis

Filling and storage of cryogenic propellant components cooled below boiling point in rocket tanks at atmospheric pressureFEDOROV, V. I; LUK'YANOVA, E. A.Chemical and petroleum engineering. 2000, Vol 36, Num 9-10, pp 584-587, issn 0009-2355Article

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