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Development of a Chemical Oxidizer Tank Model for Hybrid Rocket Engines
Författare
Liem Dam-Quang
Last Updated
för 6 år sedan
Licens
Creative Commons CC BY 4.0
Sammanfattning
This paper documents a numerical model, developed for the McGill Rocket Team based on classical chemical thermodynamics coupled with the Trebble-Bishnoi equation of state, to solve for the oxidizer tank conditions (pressure, temperature, mole flowrate and liquid/vapour equilibrium) during the operation of a hybrid rocket. This model is modular and can be coupled to fluid mechanics and combustion chamber models for a more detailed analysis of a hybrid rocket engine.
![Development of a Chemical Oxidizer Tank Model for Hybrid Rocket Engines](https://writelatex.s3.amazonaws.com/published_ver/9013.jpeg?X-Amz-Expires=14400&X-Amz-Date=20240727T031729Z&X-Amz-Algorithm=AWS4-HMAC-SHA256&X-Amz-Credential=AKIAWJBOALPNFPV7PVH5/20240727/us-east-1/s3/aws4_request&X-Amz-SignedHeaders=host&X-Amz-Signature=625c4cfa4d073d8adb133bd8bbb3c05178d8ff2ac9a47583b9b344015f391c21)