2024
DOI: 10.1016/j.dt.2023.04.004
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New insights in nano-copper chromite catalyzing ultrafine AP: Evaluation of dispersity and mixing uniformity

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Cited by 19 publications
(13 citation statements)
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“…In addition, it can also be found that the T p0 values of CuO/AP (300.6 °C), GO/CuO/AP (301.8 °C), and CMGO/CuO/AP (299.2 °C) are significantly advanced, especially the CMGO/CuO/AP composite. The above phenomenon fully demonstrates the more obvious catalytic performance of CMGO/CuO on AP …”
Section: Resultssupporting
confidence: 51%
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“…In addition, it can also be found that the T p0 values of CuO/AP (300.6 °C), GO/CuO/AP (301.8 °C), and CMGO/CuO/AP (299.2 °C) are significantly advanced, especially the CMGO/CuO/AP composite. The above phenomenon fully demonstrates the more obvious catalytic performance of CMGO/CuO on AP …”
Section: Resultssupporting
confidence: 51%
“…It can also be found that the distribution of different elements in CMGO/CuO is denser than that of GO/CuO, especially the Cu element. The above conclusions demonstrate that CuO nanoparticles can be better combined with CMGO, resulting in a more uniform dispersion of nano-CuO on CMGO, which is related to the ATA on the surface of GO. , …”
Section: Resultsmentioning
confidence: 68%
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“…It is required to increase the burning rate and thrust of the propellants to meet the capabilities of precision guidance, long-range strike, and efficient destruction for the weapon system. At present, various solutions for improving the burning rate of solid propellants have been used, such as the application of nano-oxidants, high-energy oxidants, and so on. The above methods could significantly improve the burning rate and specific impulse of propellants but they also have fatal flaws, such as easy agglomeration and poor safety. Furthermore, nanocatalysts have been a hotspot in propellant formulation due to their excellent properties, such as increasing the burn rate, reducing the burn pressure index and characteristic signal, etc. As a commonly used oxidant, ammonium perchlorate (AP) directly affects the performance of propellants as its content in many types of propellants up to 60–90%, such as composite propellants, composite modified double base propellants, etc. , …”
Section: Introductionmentioning
confidence: 99%
“…These catalysts are used as ballistic modifiers to modify the ballistic properties of propellants. For example, metals or alloys (Al, Ni, Cu, and NiCu , ), transition-metal oxides (ZnO, CuO, TiO 2 , MnO 2 , Fe 2 O 3 , and Co 3 O 4 ), composite metal oxides (ZnCo 2 O 4 , MnFe 2 O 4 , CoCuNiFe 2 O 4 , NiCuZnCo 2 O 4 and CuZnCo 2 O 4 , NiZnFe 2 O 4 , and CuCr 2 O 4 , ), composite metal hydride, metal salts (copper alginate and cobalt alginate) and metal composites (BCC/rGO (barium–copper–cobalt oxide, rGO = graphene oxide), and BZC/rGO (BZC = BaZnCuO 3 and rGO = graphene oxide)) have been studied for their catalytic effect in the decomposition process of AP. These catalysts can effectively reduce the high-temperature decomposition (HTD) temperature of AP.…”
Section: Introductionmentioning
confidence: 99%