Study on the Thermal Decomposition of NEPE Propellant (II) -Thermal Decomposition of HMX/RDX-NEPE Propellant
Feng Zhao
Abstract
Feng Zhao
Abstract
Two simultaneous devices of the fast thermlysis reaction cell (gas reaction cell) in situ in conjunction with rapidscan fourier transform infrared spectroscopy (RSFTIR), and the solid reaction cell in situ /RSFTIR were used to measure the gas products and condensed phase products of the thermal decomposition of HMX/RDXNEPE propellant in real time. Under linear temperature increase condition, the thermal decomposition characteristics of HMX/RDXNEPE propellant was studied. On the basis of the results obtained, the thermal decomposition mechanism was discussed.
OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.
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.
Two simultaneous devices of the fast thermlysis reaction cell (gas reaction cell) in situ in conjunction with rapidscan fourier transform infrared spectroscopy (RSFTIR), and the solid reaction cell in situ /RSFTIR were used to measure the gas products and condensed phase products of the thermal decomposition of HMX/RDXNEPE propellant in real time. Under linear temperature increase condition, the thermal decomposition characteristics of HMX/RDXNEPE propellant was studied. On the basis of the results obtained, the thermal decomposition mechanism was discussed.
Key concepts: Propellant, Thermal decomposition, Fourier transform infrared spectroscopy, Decomposition, Chemistry, Infrared spectroscopy, Chemical engineering, Chemical decomposition