M-SAT Missouri University of Science & Technology SHOT II June 29 th 2012 Caleb Myers Levi Malott...
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Transcript of M-SAT Missouri University of Science & Technology SHOT II June 29 th 2012 Caleb Myers Levi Malott...
![Page 1: M-SAT Missouri University of Science & Technology SHOT II June 29 th 2012 Caleb Myers Levi Malott Keith LeGrand Matt Glascock.](https://reader035.fdocuments.in/reader035/viewer/2022062519/5697bfab1a28abf838c9b103/html5/thumbnails/1.jpg)
M-SAT
Missouri University of Science & Technology
SHOT II
June 29th 2012
Caleb Myers Levi MalottKeith LeGrand Matt Glascock
![Page 2: M-SAT Missouri University of Science & Technology SHOT II June 29 th 2012 Caleb Myers Levi Malott Keith LeGrand Matt Glascock.](https://reader035.fdocuments.in/reader035/viewer/2022062519/5697bfab1a28abf838c9b103/html5/thumbnails/2.jpg)
Purpose:- The purpose of the
payload for SHOT II is to test Bluetooth communications in a space environment
- No problems are expected but it is untested
- BlueGiga WT-11E Bluetooth data radios
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Link to M-SAT Mission
• Secondary Mission of M-SAT is to test Bluetooth in space as an inter-satellite communication tool • Blue Tooth Benefits
• Inexpensive, off the shelf communications package• Ability to test preliminary swarm-sat communications
techniques• 433 kbps baud rate• Bluetooth system able to communicate to
approximately 50m with standard antenna system
![Page 4: M-SAT Missouri University of Science & Technology SHOT II June 29 th 2012 Caleb Myers Levi Malott Keith LeGrand Matt Glascock.](https://reader035.fdocuments.in/reader035/viewer/2022062519/5697bfab1a28abf838c9b103/html5/thumbnails/4.jpg)
Mechanical/Electrical Layout of Test:• Mechanical
• Housing – 2 Foam board boxes
• Electrical• Board Design – Milled in house• Power – 8 AA rechargeable batteries per box• Thermal –No thermal protection needed
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Functional Block Diagram:
![Page 6: M-SAT Missouri University of Science & Technology SHOT II June 29 th 2012 Caleb Myers Levi Malott Keith LeGrand Matt Glascock.](https://reader035.fdocuments.in/reader035/viewer/2022062519/5697bfab1a28abf838c9b103/html5/thumbnails/6.jpg)
Final Payload Characteristics
• Mass: 1.065 kg Total
• Frequency:2.4 GHz
• CG: ~(0,0)
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Data Acquisition
• Post-Flight• AVRISPmkII
Programmer• EEPROM registers
corresponding to 2 min time increments
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Questions