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kw.\*:("Propergol sólido")

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Results 1 to 25 of 527

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Solution Combustion Synthesis of Nanosized Copper Chromite and Its Use as a Burn Rate Modifier in Solid PropellantsSATHISKUMAR, P. S; THOMAS, C. R; MADRAS, Giridhar et al.Industrial & engineering chemistry research. 2012, Vol 51, Num 30, pp 10108-10116, issn 0888-5885, 9 p.Article

Experimental investigation of fracture surface energy of a solid propellant under different loading ratesNAIT ABDELAZIZ, M; NEVIERE, R; PLUVINAGE, G et al.Engineering fracture mechanics. 1988, Vol 31, Num 6, pp 1009-1026, issn 0013-7944Article

Two asymptotic models for solid propellant combustionMARGOLIS, S. B; ARMSTRONG, R. C.Combustion science and technology. 1986, Vol 47, Num 1-2, pp 1-38, issn 0010-2202Article

One-dimensional burning wave in a bed of monopropellant particlesDREW, D. A.Combustion science and technology. 1986, Vol 47, Num 3-4, pp 139-164, issn 0010-2202Article

Determination of the temperature in a solid propellant flame by analysis of emission spectraECKL, W; EISENREICH, N.Propellants, explosives, pyrotechnics. 1992, Vol 17, Num 4, pp 202-206, issn 0721-3115Article

Modelling of two-phase transient flow and combustion of granular propellantsMARKATOS, N. C.International journal of multiphase flow. 1986, Vol 12, Num 6, pp 913-933, issn 0301-9322Article

A study of solid propellant containing titanium hydrideNAKAHARA, M; YANO, Y.Propellants, explosives, pyrotechnics. 1996, Vol 21, Num 4, pp 203-205, issn 0721-3115Article

Use of dynamic mechanical measurements to determine the aging behavior of solid propellantHUSBAND, D. M.Propellants, explosives, pyrotechnics. 1992, Vol 17, Num 4, pp 196-201, issn 0721-3115Article

Experimental method for J1C computation on fracture of solid propellants under dynamic loading conditionsNAIT ABDELAZIZ, M; NEVIERE, R; PLUVINAGE, G et al.Engineering fracture mechanics. 1987, Vol 28, Num 4, pp 425-434, issn 0013-7944Article

The A/F self modulation function and the burning rate characteristics of the fuel of an un-chocked solid fuel ramjetNAKAGAWA, I; KUWAHARA, T.Kayaku Gakkaishi. 1996, Vol 57, Num 4, pp 142-147, issn 1340-2781Article

Impact testing methods for gun propellantsVARGA, L.Propellants, explosives, pyrotechnics. 1992, Vol 17, Num 3, pp 126-130, issn 0721-3115Article

Modeling of Heterogeneous Propellant Combustion: A SurveyJACKSON, Thomas L.AIAA journal. 2012, Vol 50, Num 5, pp 993-1006, issn 0001-1452, 14 p.Article

A novel kind of solid rocket propellantLO, R. E.Aerospace science and technology. 1998, Vol 2, Num 6, pp 359-367, issn 1270-9638Article

A comprehensive analysis of laser-induced ignition of RDX monopropellantLIAU, Y.-C; KIM, E. S; YANG, V et al.Combustion and flame. 2001, Vol 126, Num 3, pp 1680-1698, issn 0010-2180Article

Compatibility of infrared band models with scatteringREED, R. A; BROWN, D. G; HIERS, R. S et al.Journal of thermophysics and heat transfer. 1994, Vol 8, Num 2, pp 208-215, issn 0887-8722Conference Paper

The degradation and stabilisation of solid rocket propellantsBUNYAN, P; CUNLIFFE, A. V; DAVIS, A et al.Polymer degradation and stability. 1993, Vol 40, Num 2, pp 239-250, issn 0141-3910Conference Paper

Experimental investigation of the characteristics of solid-propellant, velocity-coupled response functionsNARAYANASWAMI, L. L; ZINN, B. T; DANIEL, B. R et al.AIAA journal. 1987, Vol 25, Num 4, pp 584-591, issn 0001-1452Conference Paper

Numerical studies on erosive burning in cylindrical solid propellant grainSRINIVASAN, K; NARAYANAN, S; SHARMA, O. P et al.Heat and mass transfer. 2008, Vol 44, Num 5, pp 579-585, issn 0947-7411, 7 p.Article

Micropropulseur à propergol solide pour des applications spatiales : Mécanique des Fluides : microfluidique : Micro-écoulements liquides et gazeux : phénomènes physiques et applications. (2ème partie) = Solid propellant micro thrusters for space applicationLARANGOT, B; ROSSI, C; ESTEVE, D et al.Houille blanche (Grenoble). 2003, Num 5, issn 0018-6368, 5, 111-115 [6 p.]Article

Compact model based on a lumped parameter approach for the prediction of solid propellant micro-rocket performanceORIEUX, S; ROSSI, C; ESTEVE, D et al.Sensors and actuators. A, Physical. 2002, Vol 101, Num 3, pp 383-391, issn 0924-4247, 9 p.Article

Plasma propagation and ignition of propellant in the chamber of a SPTEC gunPERELMUTTER, L; GOLDENBERG, C; SUDAI, M et al.IEEE transactions on magnetics. 1999, Vol 35, Num 1, pp 213-217, issn 0018-9464, 1Conference Paper

Modification of thermal theories to solid propellant ignitibilitySU, F.-H.Propellants, explosives, pyrotechnics. 1997, Vol 22, Num 2, pp 97-103, issn 0721-3115Article

Characteristic properties of AN/GAP-propellantsMENKE, K; BÖHNLEIN-MAUSS, J; SCHUBERT, H et al.Propellants, explosives, pyrotechnics. 1996, Vol 21, Num 3, pp 139-145, issn 0721-3115Article

Estimation of aluminum in HTPB based composite solid propellants by hydrogen evolution methodAJAZ, A. G.Propellants, explosives, pyrotechnics. 1996, Vol 21, Num 4, pp 196-198, issn 0721-3115Article

Research on the crack mechanism of high-burning-rate propellant in the solid rocket motorWANG, D. A; WANG, N. F; QIN, G. M et al.Propellants, explosives, pyrotechnics. 1995, Vol 20, Num 1, pp 11-15, issn 0721-3115Article

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