| Payload | Comments | Pros | Cons | Deal breakers |
|---|
| Spinal Compression | | | | |
| Peltier Power Generation | ~ 2% Assuming Ambient nose cone temp is ~90F and nose cone wall reaches of the composites at 330F we have a 250F gradient to work off of. Extrapolating from commercial power generation units we can expect ~.4A at 3.3V with the best case temperature gradient. 1 2 COTS generators appear to be implemented to work off ~600-800 F differentials, modify COTS unit? | | | |
| Solar Irradiance Falloff Detection | Easily implemented with COTS parts. 1 Requires a window in nose cone. Window could be complicated to implement. 360 degree window and optics system or interpolation required. | | | |
| Piezoelectric Beam Damping | Engineering space poorly defined. Lack of theoretical models to design system | | | |
| Microgravity Fluid Transfer | PMD's are a PITA to design. Otherwise all COTS parts | | | |
| Reaction Wheels | Must be inhibited until after apogee for FAA/ESRA compliance. Potentially compounds/introduces vehicle risk. Closed form mathematical engineering space. | | | |
| High Altitude Gas Sampling | | | | |
| Culture Cell Flight | | | | |
| 3-axis Stabilized Camera | Requires window in nose cone. Potentially COTS unit. | | | |
| High altitude air sample - DNA sequencing | | | | |
| Radar Altimeter - IAP Class? | Homebrew radar range finder/mapping | | | |