- 2 use cases: (1) Satellite to Ground, and (2) Satellite to Satellite
- 3 core pieces: bus, payloads (crosslink control, antennae), mission processing (Linux)
- Runtime is powered on for a small duration (on demand)
- 3 tech parts: IPFS (trimmed down), content management (e.g. web server), network layer (most work needs to be done here)
- Constraints: high packet loss rates, variable bandwidth
- Sample protocol: CCSDS (Common Space Protocol) similar to IPV4
- Could take the API directly to the bus if applicable
- 128kbps bandwidth (decent amount is overhead)
We plan to have regular meetings (TBD). Non-mission data will be published in this repository.