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- The payload must be deployed from the rocket.
- The payload must conform to the 3U cubesat form factor.
- The payload must weigh at least 8.8lbs.
- Only 20% of the payload mass can be non-functional.
- The payload must be recoverable.
- The payload must have redundant recovery systems.
- The payload must land at less than 30 ft/s.
- The payload's location must be real-time tracked by ESRA Mission Control Center (MCC).
- Are we going mach? TODO
Primary Objective Requirements
Not mission critical, but top level
- example: The payload must deploy an antennathere is probably only one of these and it shouldn't change
will live stream video to the ground during flight.
Derived Requirements
Requirements derived from MC and PO requirements
- these are likely to change a lot since this decides implementationhigh visibility streamer (go tigers)
- drogue chute
- one downward facing camera
- local (non-streamed) camera upward/sideward (maybe)
- no reason to not put as many we can fit/power
- vertical would be cool (see the parachute)
- less overlapping information that downward and upward
- name idea: COTs in 4k
- we need to power the cameras
- we need a video transmitter
- 2.4 GHz vs. 5.8 GHz
- how do we get signal to the ground
- directional antenna somewhere
- cool modulation - spreading sequence, something else
Secondary Objective Requirement(s)
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