ROCKÉTS

The fastest club at ÉTS

RockÉTS is a rocketry science club at École de Technologie Supérieure. The club has more than 40 students from all engineering branches that are passionate about space and science. RockÉTS's mission is to share our knowledge, as well as our motivation to everyone around us. To make this happen, we participate in several events and gatherings for all different age and interest groups.

More particularly, we represent ÉTS at the annual Spaceport America Cup competition. This competition takes place in Las Cruces, New Mexico, in the beginning of June. During this event, we share and celebrate the work done throughout the year with other rocketry clubs from around the world and anyone who are interested in seeing an aerospace show.

Finally, RockÉTS is proud to contribute to the developement of the future aerospace industry. We seek to push our limits and continue our journey with advancements with the help from our partners

Rockets

Summary

Name Year
Amarok II 2017
Status
Recovered
Peak Altitude Peak Velocity
9466ft 899ft/s

Nose Cone

Student modified

Manufacturer
Rocketry Warehouse
Type
Von Karman Shape 5.5:1
Material
Fiberglass
Payload
360° Camera
Calibration Mass

Airframe

Student built

Main tube material
S2 Fiberglass
Booster tube material
Cycom 5320 Carbon Fiber
External diameter Internal diameter
5.16in 5.00in
Fuselage length
171in

Recovery System

Student modified

Recovery Method
Single Deployment
Reefed State
Ejection System
Airbag Inflators
Parachute Design
Icarus Canopies Nano 106
Area Main Deployment
106in² 2000ft
Descent rate Max Allowed Weight
19.0ft/s 140lb

Avionics

Student built

Module Dimensions Telemetry range
3.5in x 16in 40 000ft
Radio module
RFD900 900MHz
Avionics module power supply
24hrs LFP battery
Redundancy altimeter
Stratologger CF
Inertial Station MTi-1 series from XSens
Roll/Pitch (Dynamic) 1.0° RMS
Yaw (Dynamic) 2° RMS
Gyroscope range Accelerometer
±2000°/s ±16g

Fins

Student built

Material
Cycom 5320 Carbon Fiber
Fin flutter Binding agent
2.425Mach Epoxy

Engine

Commercial

Cesaroni Technology
PRO 98N2850-P
Maximum thrust Total impulse
759lb 3094.94lb/s
Burn time
4.9s

Summary

Name Year
Amarok III 2018
Status
Crash landing
Peak Altitude Peak Velocity
9264ft 916ft/s

Nose Cone

Student modified

Manufacturer
Rocketry Warehouse
Type
Von Karman Shape 5.5:1
Material
Fiberglass
Payload
360° Camera (WiFi stream)
Calibration Mass

Airframe

Student built

Main tube material
S2 Fiberglass
Booster tube material
Cycom 5320 Carbon Fiber
External diameter Internal diameter
5.16in 5.00in
Fuselage length
171in

Recovery System

Student modified

Recovery Method
Single Deployment
Reefed State
Ejection System
Airbag Inflators
Parachute Design
Disk Gap Band
Diameter Main Deployment
120in 1400ft
Descent rate
20.2ft/s

Avionics

Student built

Module Dimensions Telemetry range
2.8in x 12.5in 40 000ft
Radio module
RFD900+ 900MHz
Avionics module power supply
24hrs LFP battery
Redundancy altimeter
Stratologger CF
Inertial Station MTi-1 series from XSens
Roll/Pitch (Dynamic) 1.0° RMS
Yaw (Dynamic) 2° RMS
Gyroscope range Accelerometer
±2000°/s ±16g

Fins

Student built

Material
Cycom 5320 Carbon Fiber
Fin flutter Binding agent
2.37Mach Epoxy

Engine

Commercial

Cesaroni Technology
PRO 11077 N2600-P
Maximum thrust Total impulse
685.1lb 2490.3lb/s
Burn time
4.28s

Summary

Name Year
Ookpik 2018
Status
Lost in the desert
Peak Altitude Peak Velocity
30 576ft 1760ft/s

Nose Cone

Student modified

Manufacturer
Rocketry Warehouse
Type
Von Karman Shape 5.5:1
Material
Fiberglass
Payload
Accelerometer

Airframe

Student built

Main tube material
Cycom 5320 Carbon Fiber
S2 Fiberglass
Booster tube material
Cycom 5320 Carbon Fiber
S2 Fiberglass
External diameter Internal diameter
4.20in 4.00in
Fuselage length
156.5in

Recovery System

Student modified

Recovery Method
Single Deployment
Reefed State
Ejection System
Airbag Inflators
Parachute Design
Disk Gap Band
Diameter Main Deployment
84in 1500ft
Descent speed
20.2ft/s

Avionics

Student built

Module Dimensions Gyroscope range
2.8in x 12.5in ±2000°/s
Telemetry range Accelerometer
40 000ft ±16g
Broadcasting Module
RFD900+ 900MHz
Redundancy altimeter
Stratologger CF
Payload
RPi Fisheye camera

Fins

Student built

Material
Cycom 5320 Carbon Fiber
Manufacturing Process
Single-piece fin canister
Fin flutter
2.37Mach

Engine

Commercial

Cesaroni Technology
PRO 98 19318N3301-P
Maximum thrust Total impulse
1141.1lb 4342.64lb/s
Burn time
5.86s

Team

Alex Boivin Captain Mechanical Engineering
Cyril Pauck-Therrien Co-captain Mechanical Engineering
Jean-Simon Thibodeau Aerodynamics Director Mechanical Engineering
David Bourgault Avionics Director Software Engineering
Hugo Lussier Treasurer Mechanical Engineering
Alexa Cruz Communications Director Mechanical Engineering
Gabriel Perron Propulsion Director Mechanical Engineering

Thanks to all of our partners

Commanders

Pilot

Specialists

Engineers

Astronauts

Expert

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