Space Systems
Orbital Mechanics, Smallsat Architecture & Satellite Operations
Quantrix Space Systems engineers next-generation computational architectures and mission-aware physical systems for low-Earth orbit (LEO), geostationary transfer (GEO), and deep-space telemetry. We focus on compressed bus integration, autonomous station-keeping, and deterministically verified orbital guidance that bypasses traditional ground-station communication bottlenecks.
Key Capabilities & Envelopes
Autonomous Station-Keeping
Closed-loop orbital GNC algorithms compensating for solar radiation pressure and J2 atmospheric drag without ground intervention.
Smallsat Constellation Bus
Standardized 12U/16U CubeSat avionics integrating radiation-hardened microcontrollers and redundant CAN-bus telemetry.
High-Bandwidth S/X Downlink
Deterministic phase-array beam steering engineered for gigabit sensor downlink during 4-minute LEO horizon passes.
Live Physics & Telemetry Model
Interact with real-time mathematical derivations and environmental envelopes specific to Space Systems.
Core Subsystem Specifications
Orbital Dynamics & Trajectory Kernel
High-fidelity orbital propagation engine accounting for high-order gravity harmonics and third-body perturbations.
Smallsat Power & Thermal Conditioning
Direct-dissipation thermal heat-pipes with MPPT gallium-arsenide solar array power management.
Radiation-Hardened Telemetry Interface
Triple-modular redundant (TMR) fault-tolerant memory controller with automated single-event latchup (SEL) power-cycling.
Defense & Aerospace Standards Matrix
ECSS-E-ST-10C
Space Engineering Systems
NASA-STD-8739.4
Avionics Interconnects
DO-178C Level A
Flight Critical Software
MIL-STD-1553B
Digital Time-Division Data Bus