Rocketry

The UTAT Rocketry division has a mission to develop expertise in the design of high-altitude sounding rockets. We accomplish this in three fields of rocketry by developing hybrid, liquid, and solid engined rockets at a variety of scales.

Project Overview

Defiance

Achievements and Records

With the Defiance series, UTAT Rocketry holds a series of records:

  • First experimental hybrid launch in Canada - flown in August 2022. Achieved an apogee 21,000 ft at the inaugural Launch Canada competition

  • Highest altitude Student Research and Developed (SRAD) advanced engine in Canada. Achieved an apogee of 30,500 ft and top speed of Mach 1.4 at Launch Canada 2024

And has earned podium places at Launch Canada, three years in a row:

  • First Place in the Advanced Category - LC2022

  • Third Place in the Advanced Category - LC2023

  • Second Place in the Advanced Category - LC2024

Defiance is a hybrid-propellant rocket that UTAT has been developing since 2017, with a target altitude of 30,000 ft. Defiance uses parachute recovery and has several telemetry modules which relay GPS coordinates from the nose cone and avionics bay of the rocket to the ground station operators. The entire project and the necessary infrastructure to operate it (such as cold flow and hot fire engine test stands) have been developed, built, and tested by UTAT Rocketry.

Originally, Defiance was designed for an altitude of 60,000 ft, aiming to break the Canadian amateur rocketry altitude record with a hybrid. We later decided through various testing results that the aspect ratio of such a slender rocket would not be structurally viable, and we decided to reduce the rocket's length and consequently the altitude target.

In the end, we broke a different kind of record, achieving the first experimental hybrid rocket flown in Canada.

This is an incredible achievement for the University of Toronto. It took a monumental effort from everyone involved and the invaluable effort of the University of Toronto Institute of Aerospace Studies, UTIAS, who provided us with the facilities and space needed to test and build Defiance. It was truly a project that redefined limits!


Vehicle Architecture

  • Rocket Name: Defiance

  • Vehicle Configuration: Single Stage

  • Propulsion System: N₂O / Paraffin Hybrid Engine

  • Propellant Load: 16.9 kg N₂O Oxidizer / 3.8 kg Paraffin Wax Fuel Core

  • Total Impulse: 38,428 Ns

  • Airframe Length: 546 cm / 215 in

  • Airframe Diameter: 14 cm / 5.5 in

  • Dry Mass: 39.61 kg / 87.32 lbs

  • Wet Mass: 61.89 kg / 136.4 lbs

Nosecone

  • 6-ply fibreglass construction

  • The nosecone is connected to the recovery system by a bulkhead and eye nut at its shoulder. The bulkhead can be removed to access the payload volume.


Recovery Bay

  • 10-ply carbon fibre construction

  • Section of the airframe housing all of the recovery hardware. The recovery system is connected to the vehicle by an eye nut at the bottom of the bay.


Avionics Bay

  • 15-ply 3 mm fibreglass tubes construction

  • Section of the airframe housing the two COTS flight computers, radio, GPS and power supply.


Fill Bay

  • 10-ply carbon fibre construction

  • Section of the airframe housing the engine fill system. The bay houses the plumbing and actuators used to load the oxidizer tank with propellant. It also contains a N2 bottle used to pressurise the tank.


Oxidizer Tank

  • Al 6061-T6 construction with a wall thickness of 3.175 mm

  • The oxidizer tank holds the N₂O oxidizer at 800 psig during and before the burn. It is loaded through the Fill Bay which is connected to the fill system on the ground.


Combustion Chamber

  • Al 6061-T6 construction with a wall thickness of 3.175 mm

  • The combustion chamber contains the paraffin wax fuel core. Oxidizer is fed through a shower head injector at the top.


Fin Can / Boat Tail

  • Fin Can: 4-ply carbon fibre construction

  • Houses a graphite nozzle for the engine. The fins provide a stability margin of 4.1 cal.

Discovery

Discovery is the team’s first-ever liquid propellant rocket. This project aims to grow our expertise in liquid engine development, with the ultimate goal of developing a liquid rocket that can breach the Karman line, reaching the edge of space. Discovery has a target altitude of 10,000 ft and will serve as a stepping stone toward future high-altitude liquid projects.

Solid Rocket Certification Program

One of our key initiatives is a solid rocket certification program, which trains our members with basic rocketry and prepares them for engaging more thoroughly with the team.

Team Structure

Team Leadership

  • Joséa Tarulli

    Director of Rocketry

  • Liam Xue

    Liquid Chief Engineer

  • Bhakti Chohan

    Hybrid Chief Engineer

  • Rodrigo Salazar

    Hybrid Project Manager

  • Timo Lahteenmaa-Swerdlyk

    Solid Project Manager

  • Lianne Choong

    Operations Manager

  • Will Taylor

    Liquid Systems Project Manager

Rocketry Leads

  • Nat Espinosa

    Aerodynamics Lead

  • Nadim Hatoum

    Aerodynamics Lead

  • Jocelyn Wall

    Airframe Lead

  • Jack A Amodeo

    Airframe Lead

  • Abdul Asa'd

    Hybrid Propulsion Lead

  • George Chen

    Hybrid Propulsion Lead

  • Kaida Xu

    Recovery Lead

  • Akhil Ambardekar

    Liquid Propulsion Lead

  • Yubo Wang

    Liquid Propulsion Lead

  • Julia Xu

    Structures Lead

  • Joao Pedro Boaventura

    Structures Lead

  • Aspen Erlandsson

    Avionics Leads

  • Jessie Lin

    Avionics Lead

  • Jaival Patel

    Software Lead

Portfolio Leads

  • Mashoodah Patel

    Business Development Specialist

  • Kira Modylevsky

    Logistics Specialist

  • Sabiha Ahmad

    Brand & Media Specialist

  • Kota Yamakawa

    Finance Specialist

  • Eryn Richardson-Bartha

    Outreach Liaison

  • Talon De Freitas

    Chief Safety Officer

  • Oliver Harrison

    Secondary Safety Officer