Evaluation of Mono and Bimetallic Ferrocene-Based 1,2,3-Triazolyl Compounds as Burning Rate Catalysts for Solid Rocket Motor
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Heterobimetallic Catalysts for the Thermal Decomposition of Ammonium Perchlorate: Efficient Burning Rate Catalysts for Solid Rocket Motors and Missiles
Recent progress on ferrocene-based burning rate catalysts for propellant applications - ScienceDirect
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Recent progress on ferrocene-based burning rate catalysts for propellant applications - ScienceDirect
Recent progress on ferrocene-based burning rate catalysts for propellant applications - ScienceDirect
Recent progress on ferrocene-based burning rate catalysts for propellant applications - ScienceDirect
PDF) Recent progress on ferrocene-based burning rate catalysts for propellant applications
Evaluation of Mono and Bimetallic Ferrocene-Based 1,2,3-Triazolyl Compounds as Burning Rate Catalysts for Solid Rocket Motor
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