Group: Adeline, Emily, and Zaire

Correlation Missions: 

Moving towards:

Instruments/Sensors: Thermal Camera + Imager 

Cost analysis:

Size Analysis:


Why it would be interesting to pursue:



Payload Compatibility

Feature3U CubeSat (Challenging)6U CubeSat (Ideal)
Payload VolumeApprox 1.5U to 2U max.Approx 3U to 4U max.
Mass BudgetMax approx 1-2 kg for combined payload.Max approx 4-7 kg for combined payload.
Power BudgetLow Orbit Average Power (OAP), typically 10-20 W max.Higher OAP, typically 20-40 W max.
Instrument PerformanceMust accept lower spectral/spatial resolution; potentially passive (non-cryocooled) thermal imaging.Allows for higher resolution, larger optics, and active (cryocooled) thermal imaging.
Data DownlinkLower rate (e.g., 9.6 kbps VHF/UHF), limiting data collected.Higher rate (e.g., up to 4.3 Mbps S-band), supporting large science data files.