ROCKÉTS

Le club le plus rapide de l'ÉTS

RockÉTS est le club scientifique de fuséonautique de l’École de Technologie Supérieure. Composé par plus de 40 étudiants de tous les génies passionnés par l’espace et les sciences aérospatiales, RockÉTS a comme mission de partager nos connaissances, ainsi que notre motivation à tous ceux qui nous entourent. Dans ce but, nous participons à plusieurs événements et rassemblements pour tous les types de public.

Notamment, nous représentons l’ÉTS à la grande compétition annuelle du « Spaceport America Cup » qui se déroule à Las Cruces, Nouveau-Mexique, au début du mois de juin. Pendant ce dernier, nous partageons et célébrons le travail accompli pendant toute l’année en compagnie des divers clubs de fuséonautique des quatre coins du monde et tous ceux qui veulent profiter d’un spectacle aérospatial inoubliable.

Finalement, RockÉTS est ravi de contribuer à la relève du futur dans les domaines aérospatiaux. Nous cherchons à pousser nos limites et à continuer notre parcours en compagnie des avancements technologiques et de ceux qui nous appuient tous les jours.

Fusées

Summary

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

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

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

Nose Cone

Student modified

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

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

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

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

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

Nose Cone

Student modified

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

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

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

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

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

Nose Cone

Student modified

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

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

Engine

Commercial

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

Summary

Name Year
Aarluk 2019
Status
Recovered
Peak Altitude Peak Velocity
25 261ft TBDft/s

Avionics / ᐊᓂᕐᓂᕐᒃ

Student built

Module Designs
ACQUI / COMM / MISSION
MOTHERBOARD
Microcontroller RTO
STM32F407 FreeRTOS
Radio Modem IMU
RFD900x XSens MTi-3
Power supply
8xLG 18650HE4
Wireless Activation
Bluetooth (Rigado R41Z)

Payload

Student built

Objective
Measure reservoir volume via pressure difference
Ejection
Apogee separation
reefed parachute
Sensor
Honeywell PX3 Sealed gauge 15-100psi

Fins

Student built

Material
Cycom 5320 Carbon Fiber
Manufacturing Process
Single-piece fin canister
Fin flutter
1.84Mach

Nose Cone

Student modified

Manufacturer
MadCow Rocketry
Type
Ogive 4:1
Material
Fiberglass

Recovery System

Student modified

Recovery Method
Single Deployment
Reefed State
Ejection System
Airbag Inflators
Parachute Design
Iris Ultra Compact
Diameter Main Deployment
120in 450m
Descent speed
18ft/s

Airframe

Student built

Main tube material
Cycom 5320 Carbon Fiber
Booster tube material
Cycom 5320 Carbon Fiber
S2 Fiberglass
External diameter Internal diameter
6.16in 6.0in
Fuselage length
10.6ft

Engine

Commercial

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

Prix

3e Spaceport America Cup, 2019

2e place, 30 000 pieds propulsion commerciale

1re Spaceport America Cup, 2017

Prix Dr. Gil Moore pour l'innovation

11e IREC, 2016

1re place, catégorie de base Prix Jim Furfaro pour l'excellence technique

10e IREC, 2015

2e place, catégorie avancée

9e IREC, 2014

2e place, catégorie avancée 2e place, catégorie de base

8e IREC, 2013

2e place, catégorie de base

Merci à tous nos partenaires

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