![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=20240727T115204Z&X-Amz-Algorithm=AWS4-HMAC-SHA256&X-Amz-Credential=AKIAWJBOALPNFPV7PVH5/20240727/us-east-1/s3/aws4_request&X-Amz-SignedHeaders=host&X-Amz-Signature=7efe406ca4e872fbf2a90b0daa89d061c0644f6fe9b2e4ee0335b2f3706791a8)
Development of a Chemical Oxidizer Tank Model for Hybrid Rocket Engines
Author
Liem Dam-Quang
Last Updated
před 6 lety
License
Creative Commons CC BY 4.0
Abstract
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=20240727T115204Z&X-Amz-Algorithm=AWS4-HMAC-SHA256&X-Amz-Credential=AKIAWJBOALPNFPV7PVH5/20240727/us-east-1/s3/aws4_request&X-Amz-SignedHeaders=host&X-Amz-Signature=7efe406ca4e872fbf2a90b0daa89d061c0644f6fe9b2e4ee0335b2f3706791a8)