Hydroxy-terminated polyether binders for composite rocket propellants
Propellants based on cross-linked Hydroxy Terminated PolyEther (HTPE) binders are being used as alternatives to Hydroxy Terminated PolyButadiene (HTPB) compositions. HTPE propellants have similar mechanical properties to HTPB propellants but they give a less severe response in ‘slow cook-off’ tests for IM compliance. A literature review is presented on
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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
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Composite Solid Rocket Propellant Aging: Multi Parameter Statistical Analysis
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Study on Composite Solid Propellants for Rocket Assisted Projectile
Kyung-Moo Kim +2 more
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Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]
Chmielarek M +2 more
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Flexible Three-Dimensional Stress Sensor for Embedded Monitoring of Solid Rocket Propellant. [PDF]
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Numerical Simulation of Failure Modes of Solid Propellants with Internal Cavities Under Various Loading Conditions. [PDF]
Liu K, Yang Q, Cao L, Wang J, Cao P.
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Advanced Nanomaterials and Energetic Application: Experiment and Simulation. [PDF]
Pang W, Trache D, Zhang K.
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Experimental Study on the Evolution of Mechanical Properties and Their Mechanisms in a HTPB Propellant Under Fatigue Loading. [PDF]
Feng F +5 more
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