# Objective 4, Level 1 Reference # 4.1 Our Satellite shall have an internal heater powered by 9V batteries 4 that shall heat the satellite for the duration of the flight. 4.2 Our satellite shall have ½ inch foam insulation on the interior of the 4 structure. # Objective 5, Level 1 Reference # 5.1 Our Satellite have an external and internal temperature sensor 5 that shall continuously collect data for the duration of the flight. 5.2 Our satellite shall have a pressure sensor that shall continuously 5 collect external pressure data for the duration of the flight. 5.3 Our satellite shall have an internal humidity sensor that shall collect 5 data continuously for the duration of the flight 5.4 Our satellite shall have a 3 axis accelerometer that shall collect data 5 continuously for the duration of the flight. 5.5 All data collected from the temperature sensors, pressure sensor, 5 humidity sensors, and accelerometer shall be stored on a 2 GB SD card. 5.6 Data collected form the temperature sensor, pressure sensor, and 5 accelerometer be used to determine the altitude of our satellite as a function of time. # Objective 6, Level 1 Reference # 6.1 Construction and Soldering equipment shall be used only in the 6 proper manner and for the direct purpose of constructing our satellite. 6.2 All construction equipment and soldering tools shall be properly 6 stored. # Objective 7, Level 1 Reference # 7.1 The structure of our satellite be made of foam core and shall be 7 held together using aluminum tape and hot glue. 7.2 Our satellite’s structure shall remain intact during the entire flight, 7 including the ascent, the balloon burst, the descent and 7.3 All of our satellite’s sensors, cameras, and Arduino boards be 7 functioning during the duration of the flight and after landing. 3.0 Design In order to take 3D images during our flight, our camera shall flight two Canon SD 780 cameras side by side, as well as a GoPro camera. In addition, we will fly a gyroscope to collect data on the spin rate an
# Objective 4, Level 1 Reference # 4.1 Our Satellite shall have an internal heater powered by 9V batteries that shall heat the satellite for the duration of the flight. 4 4.2 Our satellite shall have ½ inch foam insulation on the interior of the structure. 4 # Objective 5, Level 1 Reference # 5.1 Our Satellite have an external and internal temperature sensor that shall continuously collect data for the duration of the flight. 5 5.2 Our satellite shall have a pressure sensor that shall continuously collect external pressure data for the duration of the flight. 5 5.3 Our satellite shall have an internal humidity sensor that shall collect data continuously for the duration of the flight 5 5.4 Our satellite shall have a 3 axis accelerometer that shall collect data continuously for the duration of the flight. 5 5.5 All data collected from the temperature sensors, pressure sensor, humidity sensors, and accelerometer shall be stored on a 2 GB SD card. 5 5.6 Data collected form the temperature sensor, pressure sensor, and accelerometer be used to determine the altitude of our satellite as a function of time. 5 # Objective 6, Level 1 Reference # 6.1 Construction and Soldering equipment shall be used only in the proper manner and for the direct purpose of constructing our satellite. 6 6.2 All construction equipment and soldering tools shall be properly stored. 6 # Objective 7, Level 1 Reference # 7.1 The structure of our satellite be made of foam core and shall be held together using aluminum tape and hot glue. 7 7.2 Our satellite’s structure shall remain intact during the entire flight, including the ascent, the balloon burst, the descent and 7 7.3 All of our satellite’s sensors, cameras, and Arduino boards be functioning during the duration of the flight and after landing. 7 3.0 Design In order to take 3D images during our flight, our camera shall flight two Canon SD 780 cameras side by side, as well as a GoPro camera. In addition, we will fly a gyroscope to collect data on the spin rate an
Team%2001%20DD%20Rev%20D%202012.docx