Thermal Decomposition Properties of Hydrogen Storage Alloy/AP/HTPB Propellants
Zhen Ge
Abstract
Zhen Ge
Abstract
Thermal decomposition properties of hydrogen storage alloy/AP/HTPB propellants are studied by TGDTG,DSC and kinetics analysis methods.The results show that compared to Al/AP/HTPB propellant,the thermal decomposition temperature of hydrogen storage alloy/AP/HTPB propellant is low,and its heat release is high;the condensed phase reaction degree of A20/AP/HTPB propellant is increased by 2.44%,whereas the thermal decomposition activation energy(Kissinger method)of its second and third temperature zone is decreased by 4.06% and 22.63%,respectively;the condensed phase reaction degree of A30/AP/HTPB propellant is increased by 10.61%,whereas the thermal decomposition activation energy(Kissinger method)of its second and third temperature zone is decreased by 30.89%and 38.87%,respectively.It was found that there is a catalytic effect of hydrogen storage alloy on the thermal decomposition of AP/HTPB propellant,and the catalytic effect inereased with an increase in the content of(Mg0.45Ni0.05B0.5Hx).
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Thermal decomposition properties of hydrogen storage alloy/AP/HTPB propellants are studied by TGDTG,DSC and kinetics analysis methods.The results show that compared to Al/AP/HTPB propellant,the thermal decomposition temperature of hydrogen storage alloy/AP/HTPB propellant is low,and its heat release is high;the condensed phase reaction degree of A20/AP/HTPB propellant is increased by 2.44%,whereas the thermal decomposition activation energy(Kissinger method)of its second and third temperature zone is decreased by 4.06% and 22.63%,respectively;the condensed phase reaction degree of A30/AP/HTPB propellant is increased by 10.61%,whereas the thermal decomposition activation energy(Kissinger method)of its second and third temperature zone is decreased by 30.89%and 38.87%,respectively.It was found that there is a catalytic effect of hydrogen storage alloy on the thermal decomposition of AP/HTPB propellant,and the catalytic effect inereased with an increase in the content of(Mg0.45Ni0.05B0.5Hx).
Key concepts: Propellant, Thermal decomposition, Materials science, Activation energy, Decomposition, Alloy, Hydrogen storage, Phase (matter)