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Rocket/Aircraft C-226C Information - Canadian Internet Rocketry Network

Horus(C-226C) Aircraft Detail
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Rocket/Aircraft Details
Name: Horus
Aircraft Type: Rocket
Manufacturer : Andre Choquette
Model: Custom




Aircraft Configuration Details
    Original Configuration   
 
Original Configuration (Default/Original Configuration )
General Details
Constructed/Completed: 2011/06/24
Config. Status: Operational
Dimensions
Height: 116.14in
Payload bay: 11.81in
Diameter: 6.14in
CP: 89.72in from tip
Dry weight : 16.03kg
Materials
Fins: Fiberglass
Body: Fiberglass
Misc. Parameters
* Special purpose electronics
Motor Mount Definition  
Main Stage:
1 x 98mm, Retention ring (eg: Aeropack, Slimline)
Recovery Definition  
Recovery event 1 configuration:
Altimeter (Apogee)
Backup: Altimeter (Apogee w/Delay)
1 x 23.62in. Dome chute

Recovery event 2 configuration:
Altimeter (Altitude) Alt. (Def.): 984.25ft
Backup: Altimeter/Timer (Delay)
1 x 177.56in. Dome chute

L4 Certification