Combustion behaviour of composite propellant at sub-atmospheric pressureSCHOYER, H. F. R; KORTING, P. A. O. G.Acta astronautica. 1986, Vol 13, Num 2, pp 55-61, issn 0094-5765Article

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

Activated charcoal - A novel burn rate enhancer of aluminized composite propellantsVERMA, Sumit; RAMAKRISHNA, P. A.Combustion and flame. 2010, Vol 157, Num 6, pp 1202-1210, issn 0010-2180, 9 p.Article

Burning characteristics of ammonium perchlorate-based composite propellant supplemented with diatomaceous earthSHIOYA, Shingo; KOHGA, Makoto; NAYA, Tomoki et al.Combustion and flame. 2014, Vol 161, Num 2, pp 620-630, issn 0010-2180, 11 p.Article

Modeling the moisture effects of solid ingredients on composite propellant propertiesMUHAMMAD MAZHAR IQBAL; WANG LIANG.Aerospace science and technology. 2006, Vol 10, Num 8, pp 695-699, issn 1270-9638, 5 p.Article

CHEMICAL ENGINEERING IN SOLID PROPELLANT INDUSTRY.MURTHY JSN.1976; CHEM. ENGNG WORLD; INDIA; DA. 1976; VOL. 11; NO 12; PP. 67-70; BIBL. 7 REF.Article

RECHERCHE ET DEVELOPPEMENT SUR LES PROPERGOLS COMPOSITES DES SYTEMES DE PROPULSION DE FUSEE SOLIDES AU JAPONTODA Y.1982; KOGYO KAYAKU. (JOURNAL OF THE INDUSTRIAL EXPLOSIVES SOCIETY, JAPAN); ISSN 0368-6450; JPN; DA. 1982; VOL. 43; NO 6; PP. 353-359; ABS. ENGArticle

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

Modélisation de la combustion normale et érosive des propergols composites = Modelization of normal and erosive combustions of composite propellantsGODON, Jean-Claude.1983, 192 fThesis

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

Caractéristiques de combustion de propergols composites à base de nitraminesNAKATSUKA, K; SUMIKAWA, K; SUZUKI, N et al.Kogyo Kayaku. 1984, Vol 45, Num 6, pp 357-361, issn 0368-6450Article

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

A MASS-SPECTROMETRIC INVESTIGATION OF THE CHEMISTRY OF PLATEAU BURNING PROPELLANTS.FARBER M; SRIVASTAVA RD.1978; COMBUST. AND FLAME; USA; DA. 1978; VOL. 31; NO 3; PP. 302-323; BIBL. 26 REF.Article

BREVET 2.360.537 (A1) (77 12308). - 22 AVRIL 1977. PROPERGOL SOLIDE ET SON PROCEDE DE PREPARATION.sdPatent

PHENOMENES DE COMBUSTION DE PROPERGOLS SOLIDES. IVKUBOTA N.1980; KOGYO KAYAKU; ISSN 0368-6450; JPN; DA. 1980; VOL. 41; NO 5; PP. 255-261; ABS. ENGArticle

IGNITION OF COMPOSITE SOLID PROPELLANTS BY THE HOT PLATE TECHNIQUE.GIRDHAR HL; ARORA AJ.1978; COMBUST. AND FLAME; USA; DA. 1978; VOL. 31; NO 3; PP. 245-250; BIBL. 9 REF.Article

EXPERIMENTAL STUDY ON OSCILLATORY COMBUSTION IN SOLID-PROPELLANT MOTORS.KOREKI T; AOKI I; SHIROTA K et al.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 9; PP. 534-539; BIBL. 9 REF.Article

TRANSIENT COMBUSTION RESPONSE OF AP/HTPB COMPOSITE PROPELLANT TO ACOUSTIC OSCILLATIONS IN A ROCKET MOTORWEIDONG CAI; THAKRE, Piyush; VIGOR YANG et al.Combustion science and technology. 2009, Vol 181, Num 4-6, pp 597-617, issn 0010-2202, 21 p.Article