Changes

In the forward airframe, the rocket will be split into the forward airframe avionics bay, herein referred to as the main avionics bay, and the aft airframe avionics bay, herin referred to as the secondary avionics bay. The main avionics bay will collect sensor information and communicate mission critical parts with the ground station. The unpressurized section is for the altimeter which will deploy the main parachute. The secondary avionics bay will contain an altimeter that controls the de-spin unit and drogue chute.

In the forward airframe, the rocket will be split into the forward airframe avionics bay, herein referred to as the main avionics bay, and the aft airframe avionics bay, herin referred to as the secondary avionics bay. The main avionics bay will collect sensor information and communicate mission critical parts with the ground station. The unpressurized section is for the altimeter which will deploy the main parachute. The secondary avionics bay will contain an altimeter that controls the de-spin unit and drogue chute.

[[File:Block_Diagram.png|frame|center|alt=Avionics Block Diagram|upright=0.6|Avionics block diagram]]

[[File:Block_Diagram.png|thumb|center|upright=2.0|alt=Avionics Block Diagram|Avionics Payload Diagram]]

== Avionics Teensy Pinout and XBee Transmitter ==

== Avionics Teensy Pinout and XBee Transmitter ==