Projected Apogee: 7,860 ft
Projected Top Speed: Mach 0.58
Liftoff Mass: 218 g
Inert Mass: 68 g
Propulsion System: Aerotech G12ST-P Single Use DMS Motor
Body Tube Material: Active Foaming Acrylonitrile Styrene Acrylate
Nose Cone Material: Active Foaming Acrylonitrile Styrene Acrylate
Fin Material: Active Foaming Acrylonitrile Styrene Acrylate
Next Launch: April 18, 2026
Ithaca is a low-cost, ultra-lightweight rocket seeking to approach an apogee of 10,000 ft while only using a low-power (G-class impulse) solid rocket motor.
By utilizing additive manufacturing and, more specifically, active foaming filament technology, Ithaca is able to achieve material densities below that of commercially
available kraft paper commonly used in model rockets. With the combination of a modest impulse from its Aerotech G12ST-P rocket motor and extremely low weight,
Ithaca provides a simple, economical platform for rocket enthusiasts to reach high altitudes without the need for a Level 1 certification.
Projected Apogee: 4,200 ft
Projected Top Speed: Mach 1.15
Liftoff Mass: 242 g
Inert Mass: 114 g
Propulsion System: Aerotech G80-7T Blue Thunder Motor
Body Tube Material: High Density, High Strength Paper ("Blue Tube")
Next Launch: April 18, 2026
More information coming soon...
Projected Apogee: 4,500 ft
Projected Top Speed: Mach 1.45
Propulsion System: Aerotech G80-7T Blue Thunder Motor
Body Tube Material: Acrylonitrile Styrene Acrylate
Nose Cone Material: Acrylonitrile Styrene Acrylate
Fin Material: Acrylonitrile Styrene Acrylate
Next Launch: April 18, 2026
More information coming soon...