1. MinnRock Design and Canister Layout 11-20-09

2. Team members Bryce Schaefer (team coordinator)- AEM Cameron Japuntich- AEM Liz Sefkow- ME Mitch Andrus- ME Chris Larson- ME Phillip Hoffman- EE

3. Mission Objective The MinnRock II board is a flight characterization board similar to the board that flew last year, the MinnRock (I) project. We aim to look at many aspects of the rocket’s flight, including: spin rate, 3D acceleration, light intensity, pressure, and temperature, and the Earth’s magnetic field as a function of the rocket’s altitude Spin rate with a single light sensor 3D acceleration (x, y, z) as a function of time The inner pressure and temperature within the canister The Earth’s magnetic field as a function of the rocket’s altitude The trajectory of the rocket using a GPS Other objectives Capture still pictures while in flight using a camera, and observe the possibility of switching to video mid-flight.

4. Expected Results We expect to be able to compare data from this years flight to our own existing data We wish to answer any questions regarding the use of a GPS or (video)camera

6. Solid Works images We have a full layout of our solid works slides This layout may change due to center of mass issues, and or the implementation of wiring The next few slides show our payload first as a whole, then separated into parts to show details Some components are shown as simple blocks because they are being made in-house and have not yet been created

7. MinnSpec

8. Lower Plate (from above)

9. Lower Plate (from below)

10. Upper plate (from above)

11. Electrical Schematics We have modified the schematics from RockOn! In order to integrate a camera, GPS, and magnetometer On the next slide is the modified schematic of the AVR boards

13. Subsystems overview The MinnRock II portion of the payload is split up into three specific areas: - Camera - GPS - AVR boards Each of the subsystems will be observed in further detail on the next slides

14. Camera We have recently talked with Wyoming and have decided that the optimal route for us to go is to have them utilize the optical port and take care of the camera, while we utilize the atmospheric ports with our spectroscopy experiments. We will therefore be “sharing” pictures and optical data. This means we will effectively be removing our camera from the experiment We will likely cut a space out of our tray in order to allow Wyoming ample space to center their camera on the window The question of structural integrity has been addressed with the addition of a “cut” in our plates, but any danger has been dismissed due to the presence of our steel plates

15. GPS New focus has been placed on the GPS in order to get it fully operational while integrated in our canister The antenna needs to be near the optical port, and has therefore been “hung” from our bottom tray in order to place it as close as possible to the port, and also to eliminate any interference from the steel trays This plan has been relayed to Wyoming in order to avoid the antenna bumping into the camera

16. Planned Changes to the RockOn! AVR boards Use the board to power on the video camera, which has its own battery pack and its own SD memory card. Do not wire it directly to the G-switch, lest it get turned off again during in- flight acceleration changes. Add an SD card slot to the AVR board for removable flash memory, rather than using a surface-mounted flash memory chip. Add a USB socket into which GPS will be plugged. The GPS will be powered through the USB cable and the GPS data will be returned through the USB cable, to be stored in the AVR board’s SD card. The 3-axis magnetometer chip will be wired directly to the AVR board, drawing power from the board and sending data into the AVR through 3 open input ports (port numbers TBA). The pressure sensor will be wired the same as the RockOn design, though we will use a 0-30 psi pressure sensor which will not over-range when the canister is pressurized. Rather than using a surface-mounted temperature sensor, use two standard 3-pin temperature sensors, one directly on the AVR board and the other mounted near the window and plugged into the AVR board (port numbers TBA)

17. Power Distribution SensorVoltage (V)Current (A)Power (W)Power x Quantity (W) Z-axis high range accel 5.0013.0065 Z- axis low range accel 3.00045.00135 X/Y-axis high range accel 5.0022.011 X/Y-axis low range accel 3.00045.00135 Magnetometer16200 Hz4.32 MB Temperature22100 Hz0.72 MB Pressure11100 Hz0.36 MB Light Sensors66200 Hz4.32 MB GPS

18. Data Storage Requirements SensorNumber of Sensors Number of Outputs Channels Sampling RateTotal flight Memory Accel - Low Range23300 Hz3.24 MB Accel – High Range23100 Hz1.08 MB GPS118.1838 MHz29.5 GB GPS11500 kHz900 MB Magnetometer16200 Hz4.32 MB Temperature22100 Hz0.72 MB Pressure11100 Hz0.36 MB Light Array6650 Hz1.08 MB Total Sensor Flight Memory 10.08 MB

19. Additional Comments/Concerns We would still like to get a copy of the AVR board schematics that is modifiable to fit our experiment We will constantly be updating our solid models to fit the new design constrictions