Testing of LiAlH4 as a Potential Additive to Paraffin Wax Hybrid Rocket Fuel
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Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Analysis of Combustion Characteristics of HTPB, Graphite, Aluminum, Iron, and Gaseous Oxygen-Based Hybrid Rocket Propellant;International Journal of Aeronautical and Space Sciences;2023-06-30
2. Effect of complex metal hydride on the thermal decomposition behavior of AP/HTPB-based aluminized solid rocket propellant;Journal of Thermal Analysis and Calorimetry;2022-05-02
3. Hypergolic Ignition of Lithium–Aluminum–Hydride-Doped Paraffin Wax and Nitric Acid;Journal of Propulsion and Power;2020-05
4. Preliminary Kinetic Characterization of Lithium–Aluminum Based Hydrides for Airbreathing Propulsion;Journal of Propulsion and Power;2018-01
5. Development of a 75 mm Hybrid Rocket Motor to Test Metal Additives;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22
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