1. StratoBuoy II
Matt Voll
Brian Mayernik
Pat O’Hara

2. Mission Overview
Test the hardware and software for the power system of the SpaceBuoy nanosat project
Simulate operating modes
Record telemetry
Collect data for future development of the SpaceBuoy ADCS

3. SHOT II / UN-6 Connection
Testing development hardware for SpaceBuoy
Gain understanding of operating procedures for the power system using “dummy” loads
Testing the software interfaces
Practice the use of magnetometers for use in ADCS

4. SHOT II Design and Test Details
1” foam, 11” L x 11” W x 10” H box
Reinforced foam attachments for hardware
Foil covering
Hardware:
TS-7250 embedded Linux CDH board
Prototype power board
Magnetometer configuration board
“Dummy” loads and solar panels for telemetry
Testing:
Structural testing completed
Flat-Sat testing completed
UN compliance:
Ploy-tube and necessary hardware for string attachment.
Mass: 970 g (as of June 4, 2010)

5. Expected Results Telemetry data logged from IIC devices
A-to-D for current sense & reg. voltage monitoring
Magnetometer data
Data to show simulated operating modes of SpaceBuoy

6. Demonstration Commanding interface between CDH and power board
Plot specific telemetry values (temperature, simulated operating modes, solar cell current, etc.) vs. time over the duration of the flight