||M. S. Sureshkumar, C. M. Bhuvaneswari, S. D. Kakade and M. Gupta,“Studies on the properties of EPDM-CSE blend containing HTPB for case-bonded solid rocket motor insulation”, Polymers for Advanced Technologies, Vol 19, pp.144–150, 2008.|
J. Götz,“Characterization of the structure in highly filled composite materials by means of MRI”, Propellants, Explosives, Pyrotechnics, 27(3), pp. 179–184, 2002.
J. L. Fuente and O. Rodríguez,“Dynamic mechanical study on the thermal aging of a hydroxyl-terminated polybutadiene-based energetic composite”, Journal of Applied Polymer,Vol87, pp.2397–2405, 2003.
F. Zhao, S. Heng, R.Hu, H. Gao and F. Han,“A study of kinetic behaviours of the effective centralite/stabilizer consumption reaction of propellants using a multi-temperature artificial accelerated ageing test”, Journal of hazardous materials, Vol 145, pp.45–50, 2007.
J. H.Yi, F. Q. Zhao, W. L. Hong, S. Y. Xu, R.Z. Hu, Z. Q. Chen, and L. Y. Zhang, “Effects of Bi-NTO complex on thermal behaviors, nonisothermal reaction kinetics and burning rates of NG/TEGDN/NC propellant”, Journal of hazardous materials, Vol 176, pp.257–261, 2007.
M.D.Judge,“An investigation of composite propellant accelerated ageing mechanisms and kinetics”, Propellants, Explosives, Pyrotechnics ,Vol 28, pp.114–119, 2003.
ASTM (American Society for Testing and Materials) ,“Standard Test Methods for Vulcanized Rubber and Thermoplastic Rubbers and Thermoplastic Elastomers-Tension”, American Soc. for Testing and Materials D412-98a, West Conshohocken, PA,2002.
F. M.Grafton, J. W.Carl and Huntsville.,“Liner configuration for solid propellant rocket motor”, United States Patent, 1969.
H. W.Douglass, J. H. Collins, J. S.Noel, et al.“Solid propellant grain structuralintegrity analysis”, NASA Space Vehicle Design Criteria (Chemical propulsion), NASA-SP-8073, 1973.
R. J. Amos,“Viscoelastic analysis of Cast Double Base propellant rocket motor grains”,AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit, United States, 1993.
L. H.Robert, F. M. Clyde and B. Anthony, “Rocket propellant charge and liner therefor”, United States Patent, 2780966, February 1957.
A. M. Pang, , and J. Zheng, , “Prospect of the Research and Development of High Energy Solid Propellant Technology”, Journal of Solid Rocket Technology, Vol. 27(4), pp. 289–293,2004,
G. Oertel, , Polyurethane Handbook, 2nd ed., Carl Hanser, Munich, pp.136-137,1994.
J. D. Byrd, P. B. Walters, “Case bonding considerations for large rocket motors”. AAIA 76-638,1976.
Z. P. Huang, H. Y.Nie, Y. Y Zhang, L. M. Tan, H. L. Yin, and X. G. Ma, “Migration kinetics and mechanisms of plasticizers, stabilizers at interfaces of NEPE propellant/HTPB liner/EDPM insulation”, Journal of hazardous materials, Vol 229, pp.251-257,2012.
J. A. Condon , and Osborn J. R., “The Effect of Oxidizer Particle Size Distribution on the Steady and Nonsteady Combustion of Composite Propellants”, PURDUE UNIV LAFAYETTE IND SCHOOL OF MECHANICAL ENGINEERING, 1978.
N. Wingborg,“Increasing the tensile strength of HTPB with different isocyanates and chain extenders”, Polymer Testing, 21(3), pp.283–287, 2002.
S. B. Haska, E. Bayramli, F. Pekel, and S. Ozkar,“Adhesion of an HTPB-IPDI-based liner elastomer to composite matrix and metal case”, Journal of applied polymer science, 64(12), pp.2355–2362, 1997.
H. L. Yin, Y. Wang, and D. F. Li, ,“Ingredient Migration and Their Effect on NEPE Propellant Bonding System”, Journal of Solid Rocket Technology, 32(5), pp.527-530,2009.
S. B. Navale, S. Sriraman, V. S. Wani, M.V.Manohar, and S.D.Kakade, “Effect of Additives on Liner Properties of Case-bonded Composite Propellent”, Defence Science Journal, 54(3), pp.353-359, July 2004.
S. D. Kakade, S. B. Navale, U. B. Kadam and M. Gupta,“Effect of Fillers and Fire Retardant Compound on Hydroxy-Terminated Polybutadiene-Base Insulators”, Defence Science Journal,51(2), 2001.
W. M. Albert, “Liner for solid propellant rocket motor”,United States Patent, 3446018,May 1969.
H S. Paul,“Liner composition for rocket motors comprising crosslinked carboxy terminated polybutadiene with inert filler”, United States Patent, 3855176, December 1974.
D. B. James,and T. D. Robert, “Delayed quick solid rocket motor liner”, United States Patent,4736684,April 1988.
D. B, James and T. D. Robert,“Delayed quick solid rocket motor liner”, United States Patent,4601862, July 1986.
D. B, James and T. D. Robert,“Delayed quick solid rocket motor liner”,United States Patent,4663196. May 1987.
H. G. William, E. B. Kenneth, D. B. James, and E. J. Kenneth,“Process for forming a liner and cast propellant charge in a rocket motor casing”, United States Patent, 4803019. I 989-02-07.
R. F. Bernard and E. S. Stephen,“Liner for solid propellant rocket motor”, United States Patent, 4821511, April 1989.
S. R. Gregory, F. D. Thomas and L. Timothy,“Insulating liner for solid rocket motor containing vulcanizable elastomer and a bond promoter which is a novolac epoxy or a resole treated cellulose”, United States Patent, 4956397, September 1990.
E. B. Richard and E. H. Dale,“Interpenetrating network combination of ultraviolet and thermally rocket motor liner composition and Method”, United States Patent, 5377593,January 1995.
D. E Hutchens and N.Cohen,“Low smoke rocket motor liner compositions”, United States Patent, 6051087. April 2000
W. N. Ronald, B. L. Merylin, W. P. Larry, and K. B. Elizabeth,“Erosion resistant-low signature liner for solid propellant rocket motors”, United States Patent, 6054521,April 2000.
E. W. James,“Solid propellant liner”, United States Patent,3507114, April 1970.
Anon,“Solid propellant grain structure integrity analysis”, NASA Space Vehicle Design Criteria Monograph, NASA SP-8073, 1973.
J. Gwendal, S. Phillippe and C. Costantino,“Measuring interfacial adhesion between a soft viscoelastic layer and a rigid surface using a probemethod”,The Journal of Adhesion, Vol 80,pp. 87-118 ,2004,.
K. F.Grythe and F. K. Hansen.“Diffusion rates and the fole of diffusion in solid propellant rocket motor adhesion”, Journal of Applied Polymer ,Vol 103, pp.1529-1538,2007.
Y.Y .Lin and C.Y. Hui ,“Mechanics of contact and adhesion between viscoelastic spheres: an analysis of hysteresis during loading and unloading”. Journal of Polymer Science Part B: Polymer Physics, 40(9),pp.772-793,2002,
ASTM (American Society for Testing and Materials),“Standard Test Method for Dust Explosions in a 1.2-litre Closed Cylindrical Vessel” (withdrawn 2007), ASTM E789-95, West Conshohocken, PA: American Society for Testing and Materials. 2001.
ASTM (American Society for Testing and Materials),“Standard Test Method for Minimum Explosible Concentration of Explosible Dusts”, ASTM E1515-07, West Conshohocken, PA: American Society for Testing and Materials,2007.
ASTM (American Society for Testing and Materials),“Standard Test Method for Explosibility of Dust Clouds”, ASTM E1226. West Conshohocken, PA: American Society for Testing and Materials, 2010.
W. Bartknecht, Dust Explosions: Course, Prevention, Protection, Berlin, Springer-Verlag , 1989
L. Hertzberg, and K. Cashdollar, I. Zlochower, and D. L. Ng,“Inhibition and Extinction of Explosions in Heterogeneous Mixtures”, Symposium (International) on Combustion ,20(1),1691-1700, 1985.
P. Holbrow, M. Wall, E. Sanderson, D. Bennett, W. Rattigan, and R. Bettis, Fire and Explosion Properties of Nanopowders, RR782. Buxton: UK Health and Safety Executive,2010.
S. Mannan ,3“Lee′s Loss Prevention in the Process Industries-Hazard Identification”, Assessment and Control ,Vol 2, London: Butterworth-Heinemann,1996.
M. Nifuku, and H. Katoh,“Incendiary Characteristics of Electrostatic Discharge for Dust and Gas”, Journal of Loss Prevention in the Process Industries ,14 (6),pp.547-551, 2001
F. Schuster, and J. Bouillard. NANOSAFE2: Safe Production and Use of Nanomaterials, European Project .No. 515843-2, Grenoble : MINATEC, 2005–2009.
A.Vignes, F. Muñoz, J. Bouillard, O. Dufaud, L. Perrin, A. Laurent, and D. Thomas “Risk Assessment of the Ignitability and Explosivity of Aluminum Nanopowders”, Process Safety and Environmental Protection ,90(4), pp.304-310,2012.
S. Vyazovkin and C. A. Wright,“Model-free and Model-fitting Approaches to Kinetic Analysis of Isothermal and Nonisothermal Data”, Thermochimica 340-341(1),pp.53-68,1999
H. C. Wu, H. J. Ou, H. C. Hsiao, and T, S ,Shih. “Explosion Characteristics of Aluminum Nanopowders”,Aerosol and Air Quality Research ,Vol 10,pp.38–42,2010.