Chemically Collapsible Mandrel for Solid Rocket Motor Processing
Composite propellant mainly consists of two parts, binder matrix (prepolymer, plasticizer, cross linker, antioxidant and curative etc.) and solid ingredients (oxidizer, metal fuel, burn rate modifier, combustion stabilizer etc.).
Abhijit Dey +3 more
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COMPOSITE SOLID ROCKET PROPELLANT MATERIALS
Jeffrey W. Gilman, Robert D. Chapman
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Novel Approach for the Fabrication of Composite Rocket Propellant: Increased Homogeneity and Its Influence on SRP Behaviour. [PDF]
Janowska K +5 more
europepmc +1 more source
PREPARATION AND CHARACTERIZATION OF NOVEL BINDER FOR COMPOSITE SOLID ROCKET PROPELLANT [PDF]
Hosam Mostafa, I. Kamal
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Study on Creep Mechanical Properties of HTPB Solid Propellant. [PDF]
Jin L, Jia S, Zhang Z, An Z, Lu Z.
europepmc +1 more source
Investigation on the Structural Integrity of Solid Propellant Grains with Different-Sized Void Defects. [PDF]
Wang J +6 more
europepmc +1 more source
Numerical Simulation Study on Residual Stress and Strain in the Curing and Molding of HTPB Two-Stage Solid Propellant. [PDF]
Chang J, Xu C, Dai Y.
europepmc +1 more source
Mesoscopic Damage Characteristics of NEPE Propellant Under Drop-Weight Impact. [PDF]
Zhang Z, Sun Z, Liu Y, Zhu Y, Hu Y.
europepmc +1 more source
Design and Testing of Rocket Motors with Composite Propellants
openaire +1 more source
Improving the Combustion Efficiency of Aluminum-Based Composite, Al@IL/FG, Through Surface Activation Reaction. [PDF]
Zheng QL, Huang ZL, Xu HX, Li JZ, He W.
europepmc +1 more source

