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Results 1 to 25 of 205

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Percolation model of polydisperse composite solid propellant combustionKERSTEIN, A. R.Combustion and flame. 1987, Vol 69, Num 1, pp 95-112, issn 0010-2180Article

Dynamic behavior of composites under preloadingGEISSLER, A; GEISSLER, E.Propellants, explosives, pyrotechnics. 1992, Vol 17, Num 4, pp 211-213, issn 0721-3115Article

Burning rate characteristics of energetic CMDB propellants (I) : Combustion characteristics of basic propellantAOKI, I.Kayaku Gakkaishi. 1997, Vol 58, Num 4, pp 162-168, issn 1340-2781Article

Burning rate characteristics of energetic CMDB propellants (II) : Effect of HMX additionAOKI, I.Kayaku Gakkaishi. 1997, Vol 58, Num 4, pp 169-175, issn 1340-2781Article

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

Sensitive characteristics of BAMO/NMMO/AN propellantsKAWASAKI, H; MITARAI, Y.Kayaku Gakkaishi. 1998, Vol 59, Num 1, pp 6-9, issn 1340-2781Article

Short-action solid rocket motors with double-base propellantsKENTGENS, H; MACKOWIAK, H. P; SCHÖFFL, R et al.Propellants, explosives, pyrotechnics. 1996, Vol 21, Num 3, pp 118-126, issn 0721-3115Article

Combustion mechanism of high energy composite propellants. (III) - Temperature sensivitity characteristicsBAZAKI, H; KAI, T; ANAN, T et al.Kayaku Gakkaishi. 1996, Vol 57, Num 4, pp 153-159, issn 1340-2781Article

Influence of energetic materials on the energy-output of gun propellantsVOLK, F; BATHELT, H.Propellants, explosives, pyrotechnics. 1997, Vol 22, Num 3, pp 120-124, issn 0721-3115Article

Investigation on interfacial bonding in HMX-containing model propellant compositeYAO WEISHANG; WU WENHUI; JIA ZHANNING et al.Propellants, explosives, pyrotechnics. 1995, Vol 20, Num 6, pp 327-329, issn 0721-3115Article

Analyse de l'indice de pression d'un propergol composite de perchlorate d'ammoniumMITARAI, Y.Kogyo Kayaku. 1989, Vol 50, Num 5, pp 447-451, issn 0368-6450Article

Des boosters d'Ariane 5 au gonflage des sacs Airbag : évolution d'un matériau énergétique et de son process = From Ariane 5 boosters to inflation of airbags : evolution of energetic materials and its processCHOUNET, Georges.Les cahiers de formulation. 2005, pp 84-100, isbn 2-86883-844-8, 1Vol, 17 p.Conference Paper

Ion chromatography of energetic materials at Sandia National LaboratoriesKLASSEN, S. E; MASSIS, T. M; BOESPFLUG, E. P et al.Thermochimica acta. 2002, Vol 384, Num 1-2, pp 329-341, issn 0040-6031Article

Random packing of heterogeneous propellantsKNOTT, G. M; JACKSON, T. L; BUCKMASTER, J et al.AIAA journal. 2001, Vol 39, Num 4, pp 678-686, issn 0001-1452Article

On the possibility to modify the performance of propellant mixtures used in RAMAC by addition of metallic particlesVEYSSIERE, B; INGIGNOLI, W; KHASAINOV, B. A et al.Journal de physique. IV. 2000, Vol 10, Num 11, pp Pr11.99-Pr11.107, issn 1155-4339Conference Paper

Ammonium nitrate : a promising rocket propellant oxidizerOOMMEN, C; JAIN, S. R.Journal of hazardous materials. 1999, Vol 67, Num 3, pp 253-281, issn 0304-3894Article

Preparation of Al/Zr composite powders by solid propellant combustionDEGUCHI, S.Kagaku kōgaku ronbunshū. 1995, Vol 21, Num 1, pp 126-131, issn 0386-216XArticle

Specific heats of solid gun propellantsMILLER, M. S.Combustion science and technology. 1994, Vol 102, Num 1-6, pp 273-281, issn 0010-2202Article

Species profiles in solid propellant flames using absorption and emission spectroscopyVANDERHOFF, J. A.Combustion and flame. 1991, Vol 84, Num 1-2, pp 73-92, issn 0010-2180, 20 p.Article

Sensibilité à la température initiale de la vitesse de combustion des propergols et semi-propergols solides composites à base de perchlorate d'ammonium = Initial temperature sensitivity of the combustion rate of ammonia perchlorate-based solid composite propellants and semi-propellantsFOUREST, B.La Recherche aérospatiale. 1989, Num 6, pp 67-76, issn 0034-1223, 10 p.Article

Vitesse de combustion d'un propergol solide composite en présence d'oscillations de l'écoulementPascal, Jérôme; Fitaire, Marc.1987, 234 p.Thesis

Combustion mechanism of high energy composite propellants. (V) - Combustion of azide/nitramine propellantsBAZAKI, H; IIDA, A; MITARAI, Y et al.Kayaku Gakkaishi. 1998, Vol 59, Num 1, pp 30-35, issn 1340-2781Article

Theoretical and experimental study of composite solid propellant combustionBILGER, R. W; JIA, X; LI, J. D et al.Combustion science and technology. 1996, Vol 115, Num 1-3, pp 1-39, issn 0010-2202Article

Kinetic parameters of composite propellants from thermogravimetric dataRAO, V. K; BARDON, M. F; STOWE, R. A et al.Combustion and flame. 1995, Vol 102, Num 1-2, pp 219-225, issn 0010-2180Article

Dynamic burning rate measurements of metalized composite propellants using the laser-recoil techniqueBREWSTER, M. Q; HITES, M. H; SON, S. F et al.Combustion and flame. 1993, Vol 94, Num 1-2, pp 178-190, issn 0010-2180Article

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