HiakaSat is an octagonal spacecraft with one general purpose avionics bay which utilizes single string COTS architecture. Honeycomb panel, body mounted solar panels and as-required deployable antenna(s) are baseline. Redundancy and radiation hardened component upgrades are available.
Baseline Bus Specifications
- Size/Class: MicroSat
- Mass: 50 kg
- RF Power: 10W
- ADCS Pointing: <1°
- ADCS Knowledge: <1°
- Communications: Up to 1.5 Mbps (S-band)
- Nominal Mission Lifetime: 1 year
- Design Maturity: Delivered for Launch
Payload Support
- Volume: 13 x 13 x 40 cm (internal)
- Mass: 10 kg
- Data Storage: 4 GB
- Power/Duty Cycle: 80W @ 100% duty cycle
ROM Cost
- Spacecraft: $4M
- Launch: $5M
- Operations: $1M