Development of a Chemical Oxidizer Tank Model for Hybrid Rocket Engines

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.

Liem Dam-Quang

Homework Template Fun3

Homework template for SMCM PHYS 251 Fundamentals of Physics 3 (Fun 3). Includes the Griffiths "script-r" used in many electricity and magnetism courses.

Erin De Pree

SPINS 2 Tables

Template for tables in SPINS lab 2. Used in PHYS 462 Quantum Mechanics at SMCM.

Erin De Pree

SPINS 3 Tables

Templates for tables in SPINS lab 3 for PHYS 462 Quantum Mechanics at SMCM.

Erin De Pree