The Space Systems Division develops small satellites (namely CubeSats) for space research. The team's strengths derive from its historic expertise in low-cost, modular engineering design and the development of space life science payloads. The team worked on the first iteration, HERON MK I, during 2014-16. The team decided to tackle another iteration in 2016 to improve upon the last design.
With the support of the University of Toronto (St. George) students, UTAT was able to secure a student levy to fund the launch and development of the next iteration of the cubesat, HERON MK II. The team is aiming to launch the finished cubesat in 2019.
- Structures - Responsible for all mechanical features within the satellite, including the primary and secondary payload structure, as well as the payload structural elements
- Command and Data Handling - Brain of the satellite, handling satellite control and the exchange of information and between subsystems
- Thermal - Models the spacecraft temperature over the course of an orbit, and selects materials to maintain acceptable spacecraft temperatures
- Power - Controls power generation via solar panels, and distributes this power to the other on-board systems
- Attitude Determination & Control (ADCS) - Ensures spacecraft is oriented optimally for communications, thermal loading, and power generation
- Communications - Responsible for the transmission of all data between the satellite and the ground station
- Payload - Develops and integrates the technology from which the mission purpose is derived, which in the past has included astrobiology experiments and in-space communications links
Projects & Achievements
2014-2016: HERON Astrobiology CubeSat
2017: Secured student levy across U of T campus for launch and development
This page was last updated April 7th, 2018