Phoenix 2.5

Launched / Operational

Specifications

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

Height:

Diameter: 4 in

Engine: I-class / J-class

Maximum Velocity: TBD

Expected Apogee: 1500 - 2500 ft

Recovery System: Ejection Charge, Parachute

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

Amesbury MA (10/03/2020)

Phoenix 2.5 Launch Amesbury MA

Phoenix 2.5B Lift Off

Amesbury MA (09/19/2020)

Phoenix 2.5 Launch Amesbury MA

Phoenix 2.5 Lift Off