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您的检索式：作者名="Dhirendra Gupta"
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| 1 | Burning rate and other characteristics of strontium titanate (SrTiO3) supplemented AP/HTPB/Al composite propellants显示文摘In a quest of search for a new burning rate modifier for composite propellant, strontium titanate (SrTiO3), a perovskite oxide has been chosen for evaluation in a composite propellant formulation based on its other catalytic applications. Initially, SrTiO3 was characterized for particle size, morphology and material/ phase identification (using XRD). By varying SrTiO3 content in a standard composite propellant, different compositions were prepared and their performance and processing parameters like the end of mix (EOM) viscosity, mechanical properties, density, burning rate, pressure exponent (n-value), etc. were measured. The results reveal that 2% SrTiO3 causes more than 12% enhancement in propellant burning rate (at 70 ksc pressure) in comparison to the standard propellant composition. The pressure exponent also increases to 0.46, whereas the standard composition was having its value as 0.35. | Sunil Jain Garima Gupta Dhirendra R. Kshirsagar Vrushali H. Khire Balasubramanian Kandasubramanian | 2019 | Defence Technology(防务技术)2019，15，3： | 3 |
| 2 | Investigation of passivation processes for HgCdTe/CdS structure for infrared application显示文摘 | Ragini Raj Singha Diksha Kaushika Dhirendra Gupta | 2006 | Thin Solid Films2006，510，1： | 1 |
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