01
Spacecraft Bus
A 12U-to-150 kg modular platform with deployable arrays, reaction wheels and a common payload interface across every mission class.
- Mass class
- 12 – 150 kg
- Power
- 220 W orbit average
- Pointing
- 0.02° 3-axis
Index 01 — Technology
Engineered for orbit,verified on the ground.
Every LYSR subsystem is designed, built and qualified in-house, so a mission moves from concept to downlink without waiting on a supply chain.
02
Mission Engineering
Mission analysis and subsystem integration focused on dependable spacecraft performance from launch through orbital operations.
- Analysis
- Mission focused
- Integration
- System level
- Validation
- Ground tested
03
Avionics & Flight Software
Radiation-tolerant flight computers running a fault-managed, over-the-air updatable software stack with on-board autonomy.
- Redundancy
- Dual string
- Autonomy
- Fault-managed
- Updates
- Over the air
04
Ground Segment
Twelve automated X-band and Ka-band sites hand off passes around the clock, streaming telemetry into a single mission console.
- Sites
- 12 automated
- Bands
- X · Ka · UHF
- Latency
- Sub-second
Flying a payload with us?
Tell us the mission and we'll come back with an orbit, a bus and a downlink plan.