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- W2076029079 abstract "To explain the experimental results obtained in the 30 mm Ram accelerator at ISL, showing that in the subdetonative mode, the terminal velocity of magnesium projectiles at the end of Ramac tube is higher than the CJ detonation of the propellant gaseous mixture, whereas the projectile undergoes a mass loss during the propagation, the assumption is made that metallic particles ablated from the projectile react with the gaseous species and modify the performances of the propellant mixture. The problem is examined by comparing experimental and calculation results in an analogous situation of fine aluminum particles suspended in hydrogen-air mixtures. It is demonstrated that the classical thermodynamic model is unsuitable for explaining correctly the experimental observations. Prediction of changes in performances of the propellant mixture requires that two-phase flow effects be taken into account. These changes depend on the mass concentration, size and shape of the solid particles." @default.
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- W2076029079 date "2000-11-01" @default.
- W2076029079 modified "2023-09-25" @default.
- W2076029079 title "On the possibility to modify the performance of propellant mixtures used in RAMAC by addition of metallic particles" @default.
- W2076029079 doi "https://doi.org/10.1051/jp4:20001111" @default.
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