Molecular aluminum and nitrocellulose composite additives for burn rate enhancement of liquid propellants

Engineering & Materials Science

• Agglomeration 8%
• Aluminum 47%
• Composite materials 35%
• Decomposition 7%
• Ethers 12%
• Experiments 3%
• Gases 17%
• Hot Temperature 4%
• Hydrocarbons 27%
• Ignition 9%
• Kerosene 36%
• Liquid propellants 89%
• Liquids 6%
• Mass spectrometry 26%
• Metal nanoparticles 17%
• Metals 13%
• Nanoparticles 30%
• Nitrocellulose 100%
• Oxides 8%
• Oxygen 8%
• Rate constants 38%
• Solubility 11%
• Surface active agents 11%
• Temperature 4%
• Toluene 12%
• Tuning 8%

Physics & Astronomy

• aluminum 42%
• analogs 6%
• augmentation 37%
• burning rate 10%
• cellulose nitrate 87%
• composite materials 37%
• decomposition 5%
• diethyl ether 12%
• ejection 8%
• flames 6%
• flux density 6%
• gases 11%
• heat of combustion 12%
• high speed 5%
• hydrocarbon fuels 34%
• ignition 7%
• integrity 8%
• kerosene 31%
• liquids 32%
• mass spectroscopy 15%
• metal oxides 7%
• metals 7%
• nanoparticles 20%
• oxygen 4%
• particulates 15%
• products 4%
• propellants 70%
• room temperature 4%
• solubility 7%
• surfactants 7%
• toluene 8%
• tuning 5%

Chemical Compounds

• Additive 41%
• Ambient Reaction Temperature 5%
• Calorific Value 10%
• Composite Material 30%
• Decomposition 6%
• Dioxygen 5%
• Energy 4%
• Environment 5%
• Ether 7%
• Flame 9%
• Fuel 34%
• Fuel Additive 14%
• Gas 16%
• Hydrocarbon 22%
• Kerosene 36%
• Liquid 33%
• Metal 4%
• Metal Nanoparticle 10%
• Metal Oxide 8%
• Mixture 4%
• Molecular Cluster 6%
• Nanoparticle 15%
• Nitrocellulose 72%
• Propellant 76%
• Purity 5%
• Rate Constant 20%
• Solubility 6%
• Surface 3%
• Surfactant 7%
• Time 3%
• Time-of-Flight Mass Spectrometry 20%