Interesting. The incompatibility between rocket fuel and vortex-based flight systems arises primarily due to the thermodynamic properties of conventional rocket fuels. Rocket fuels, such as liquid hydrogen (LH2) or kerosene (RP-1), are designed to undergo exothermic reactions, releasing large amounts of thermal energy that is then converted into kinetic energy to propel the rocket. However, in a vortex-based flight system, the introduction of such high-temperature reactions could lead to a phenomenon known as thermal vortex breakdown. This is a state where the core of the vortex becomes unstable due to the excessive thermal energy, causing the vortex to dissipate prematurely and thus, disrupting the lift generation process. Am I wrong in this asessment? you seem to know it better than I do
What on earth are you up to there Phil?😮
Hey mate im a mechatronic engineer let me know if you want some help with all this
Interesting. The incompatibility between rocket fuel and vortex-based flight systems arises primarily due to the thermodynamic properties of conventional rocket fuels. Rocket fuels, such as liquid hydrogen (LH2) or kerosene (RP-1), are designed to undergo exothermic reactions, releasing large amounts of thermal energy that is then converted into kinetic energy to propel the rocket.
However, in a vortex-based flight system, the introduction of such high-temperature reactions could lead to a phenomenon known as thermal vortex breakdown. This is a state where the core of the vortex becomes unstable due to the excessive thermal energy, causing the vortex to dissipate prematurely and thus, disrupting the lift generation process.
Am I wrong in this asessment? you seem to know it better than I do