Current Rockets
Mission Phobos - 2023
Wet Mass: 17.23 Kg
Dry Mass: 14.33 Kg
Outer Diameter: 10.44 cm
Inner Diameter: 10.16 cm
Length: 1.92 m
Ahmad Aldeen
Team Captain
"MetRocketry will compete in the 2023 Launch Canada Challenge with a one-stage rocket called Phobos, named after Mars’ innermost and largest moon"
"The Phobos rocket is a one-stage rocket designed for an apogee of 10,000 feet and powered by a Cesaroni Technology Inc (CTI) Commercial-Off-The-Shelf M1230 rocket motor, with an estimated launch weight of 17 Kg while flying at subsonic speed"
​Abdullah Alhuraibi
2022-2023​Propulsion Lead
​Talia de Ryck
2022-2023 Payload Lead
"The payload module for this Phobos rocket is a scientific experiment aimed at measuring Muon particles at different altitudes"
Mission Deimos - 2023
Wet Mass Mass: 29.5 kg
Dry Mass: 20.72 Kg
Outer Diameter: 10.44 cm
Inner Diameter: 10.16 cm
Length: 312.4 cm
Keiny Mugisha
2022-2023
Co-Captain
"The Phobos rocket will be the first demonstration from MetRocketry of a relaunch as Phobos will be launched in Spaceport America Cup (SAC) 2023 two months before Launch Canada (LC)"
"This year, the team decided to embark on two new projects to push its limits; relaunching a single-stage rocket (Phobos), and launching a 2-stage rocket (Deimos)"
Nsikak-Abasi Essien
2022-2023
Structures Lead
Lori Mazloomian
2022-2023
Dynamics Lead
"The rocket was designed with modularity and reliability as a significant focus, learning from past design and recovery flaws"
Rockets archives
The Ryerson Rocket - 2022
Dimensions
Propulsion
Payload
Performance
Accomplishment
The Ryerson rocket Team
Alexander Chang
Team Captain
The Ryerson Rocket is RRC's single-staged rocket. The rocket is designed and built to reach an apogee of 31,896 ft. It carries with it a scientific payload that houses a fluid compression tester integrated into the nosecone of the rocket. The payload is 8.8 lbs and carries 4 different fluids.
The rocket was demonstrated at spaceport America cup 2022. However, the rocket was not recovered successfully.
Soham Trivedi
Project Manager/ Recovery Lead
Mohamed Jundi
Aerodynamics Lead
Keiny Mugisha
Payload Lead
Alessandro Ciniello
Avionics Lead
Ahmad Ziad Zain Aldeen
Manufacturing Lead
Taruansh Qaumi
Structures Lead
Northern Lightning - 2019
Dimensions
Propulsion
Payload
Performance
Accomplishment
Northern Lightning Team
Mohammed M. KHAN
Team Captain
The Northern Lightning is Ryerson’s third Spaceport America Cup supersonic rocket. It is a sounding rocket designed for an apogee of 30000 feet.
Its design features an innovative, student researched, and developed out-of-autoclave resin transfer process which allowed for the manufacturing of high-quality supersonic fins with minimal cost, consumables, and labor
time.
Joel A. MCQUAID
Aero-structures Lead
Joel A. MOORE
Recovery Co-Lead
Jeffrey A. JEVNIKAR
Recovery Co-Lead
Luigi D. ADDANTE
Avionics Co-Lead
Trevor S. TAI
Avionics Co-Lead