One of the key molecular level characteristic of elastomeric binder systems of composite rocket propellants is the glass-rubber transition region, which is mainly defined by the molecular mobility of the components in the polymeric network during phase transition from energy to entropy elasticity with respect to temperature. This feature has a strong dependence on temperature and is detectable by dynamic mechanical analysis (DMA) whereby obtaining the loss factor (tanδ= loss module divided by storage module) curves. HTPB R45HT based binders with four different types of isocyanates (IPDI, HDI, DE305 and 6HMDI), with and without the common plasticizer DOA (dioctyl adipate), were analyzed using loss factor curves obtained by torsion DMA. Expon...
Composite rocket propellants have often three-dimensional polyurethane elastomers as binders. One of...
The oxidative thermal aging of a crosslinked hydroxy-terminated polybutadiene (HTPB)/isophorone diis...
Composite rocket propellants (CRP) contain oxidizer particles and fuel particles in an elastomeric b...
Inert non-polar HTPB binder and energetic GAP binder with polar groups are the two most common used ...
The glass-rubber transition temperature of elastomer bonded composite rocket propellants and high ex...
Recently, it was found that the second peak of the loss factor curve determined by DMA of HTPB bonde...
This study aims to evaluate the dynamic mechanical properties of a binder, used in composite propell...
International audienceThis study focuses on the viscoelastic behavior of an industrial hydroxyl-term...
Butacene® is a polymeric binder with ferrocenyl groups chemically bonded to HTPB backbone. Through i...
One of the main challenges concerning energetic materials regards the establishments and evaluations...
The aim of this work is to evaluate the effect of several types of plasticizers on the glass–rubber ...
Composite rocket propellants (CRP) have an elastomer as binder for the solid fillers, which serve as...
The glass-rubber transition (GRT) in elastomer bonded energetic material as composite rocket propell...
Hydroxyl terminated polybutadiene (HTPB) continues to be the first choice as pre-polymer for an elas...
Composite rocket propellants have often three-dimensional polyurethane elastomers as binders. One of...
Composite rocket propellants have often three-dimensional polyurethane elastomers as binders. One of...
The oxidative thermal aging of a crosslinked hydroxy-terminated polybutadiene (HTPB)/isophorone diis...
Composite rocket propellants (CRP) contain oxidizer particles and fuel particles in an elastomeric b...
Inert non-polar HTPB binder and energetic GAP binder with polar groups are the two most common used ...
The glass-rubber transition temperature of elastomer bonded composite rocket propellants and high ex...
Recently, it was found that the second peak of the loss factor curve determined by DMA of HTPB bonde...
This study aims to evaluate the dynamic mechanical properties of a binder, used in composite propell...
International audienceThis study focuses on the viscoelastic behavior of an industrial hydroxyl-term...
Butacene® is a polymeric binder with ferrocenyl groups chemically bonded to HTPB backbone. Through i...
One of the main challenges concerning energetic materials regards the establishments and evaluations...
The aim of this work is to evaluate the effect of several types of plasticizers on the glass–rubber ...
Composite rocket propellants (CRP) have an elastomer as binder for the solid fillers, which serve as...
The glass-rubber transition (GRT) in elastomer bonded energetic material as composite rocket propell...
Hydroxyl terminated polybutadiene (HTPB) continues to be the first choice as pre-polymer for an elas...
Composite rocket propellants have often three-dimensional polyurethane elastomers as binders. One of...
Composite rocket propellants have often three-dimensional polyurethane elastomers as binders. One of...
The oxidative thermal aging of a crosslinked hydroxy-terminated polybutadiene (HTPB)/isophorone diis...
Composite rocket propellants (CRP) contain oxidizer particles and fuel particles in an elastomeric b...