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Launched / Operational
Specifications
Specifications
Phoenix 2.5
Phoenix 2.5
Height:
Diameter: 4 in
Engine: H-class
Maximum Velocity: TBD
Expected Apogee: 1,750ft
Recovery System: Ejection Charge, Parachute
Phoenix 2.5 B
Phoenix 2.5 B
Height:
Diameter: 4 in
Engine: I-class / J-classÂ
Maximum Velocity: TBD
Expected Apogee: 1500 - 2500 ft
Recovery System: Ejection Charge, Parachute
Purpose
Purpose
Phoenix 2.5 was developed by our advisor Jake Felser as a test bed for our Phoenix III Avionics payload. We aim to conduct multiple flights with it in order to verify that our avionics system is reliable and can be charged with bringing our Phoenix III launch vehicle to the ground safely.
Launches
Launches
Amesbury MA (10/03/2020)
Amesbury MA (10/03/2020)
Phoenix 2.5 Launch Amesbury MA
Phoenix 2.5 Launch Amesbury MA
Phoenix 2.5B Lift Off
Phoenix 2.5B Lift Off
Amesbury MA (09/19/2020)
Amesbury MA (09/19/2020)
Phoenix 2.5 Launch Amesbury MA
Phoenix 2.5 Launch Amesbury MA
Phoenix 2.5 Lift Off
Phoenix 2.5 Lift Off
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