Notes

Mission Requirements
- Pump
- Thermal
- Servos for turning cylinder/baffles
- Sensors
- On-board computer (OBC), if necessary
- Valves for pressure release
Operational Modes
- Idle/safe mode
- Science mode
- Programming mode
- Any other modes that we so desire!
Power
- Peak current
- Peak voltage
- Duty cycle
  - Everybody should do some research into this on their own!
Protection/Reliability
- Protection from magnetic, electrical, and thermal interference
- Safety limits
- Redundancy
- "Graceful failure" - ensuring that any failures do not compromise the entire system
- Testing
- Noise reduction
- Data logs
  - Work with data management
Harnessing
- Data paths
- We need to consider any magnetic interference when we route wires. For instance, we shouldn't route wires near sensors or PCBs.
- Work with Structures to plan out harnessing in advance
On-board components
Environmental
- Account for environmental factors such as:
  - Thermal
  - Radiation
  - Electronics in a vacuum
    - Outgassing
    - Ensuring that certain components (such as capacitors) will work in a vacuum
Testing Plan
- Work with Testing & Manufacturing
Integration Plan
- Work with Oligo

Next Steps

Create block diagram(s)
Research space-rated components
- Look into radiation hardening. Do we need to do it in-house? What are our requirements for maximum radiation dosages? What about shielding thicknesses?
Communicate with other subteams to get information about sensors, servos, etc. We should compile a list of the datasheets for all of the peripherals that we need to work with.

Power Budgets
- p. 424 - SMAD
Power Subsystem
- p. 642 - SMAD
- p. 55 - LEO Satellite Design
- p. 55 - Small Spacecraft Technology SOA (the rest of the chapter before that is about power generation, less applicable to this project)
Avionics (Electronics), On-Board Processing/Computer Selection
- p. 226 - Small Spacecraft Technology SOA
- p. 601 - SMAD
- p. 87 - LEO Satellite Design
Risk and Reliability
- p. 753 - SMAD
- p. 206 - LEO Satellite Design
Radiation Hardening
- p. 203 - LEO Satellite Design
Integration and Testing
- p. 711 - SMAD
- p. 209 - LEO Satellite Design
- p. 283 - Small Spacecraft Technology SOA
Thermal Design (including managing heat from electronics)
- p. 187 - LEO Satellite Design
- p. 283 - Small Spacecraft Technology SOA
Environment
- p. 1 - LEO Satellite Design