Flight Qualified Satellite Electronics

Kepler Aerospace designs and delivers modular satellite electronics and subsystems engineered for integration readiness, operational durability, and mission reliability.

Our systems are developed for platforms up to the 200 kg class and are built with a focus on interoperability across diverse mission architectures.

We prioritize systems that are deployment-ready, not experimental prototypes.

Satellite Electronics
200kg Platform
Class Support

Communications System

Systems are engineered to support secure data transport and compatibility with modern ground architectures.

Capabilities include

SDR-based SATCOM systems
Multi-band RF receivers
Telemetry and telecommand electronics
UHF beacon systems
Ground-to-space interface compatibility

On-Board Data Handling (OBDH)

On-Board Data Handling
OBDH architecture emphasizes reliability, modularity, and seamless subsystem integration.

FPGA-Based Processing Units

Radiation-tolerant processing cores for mission-critical data management.

Space-Grade Data Acquisition

High-reliability acquisition systems designed for the space environment.

Command & Telemetry Management

Integrated handling of uplink commands and downlink telemetry streams.

Power Conditioning Electronics

Regulated power distribution and protection across all subsystem buses.

Ground Segment Electronics

Ground and space components are engineered for interoperability across the mission lifecycle.

Satellite Command & Control Platforms

Purpose-built hardware for satellite telemetry reception and command uplink operations.

Remote Mission Operations Software

Distributed operations tools enabling mission teams to manage assets from any location.

Integrated Monitoring & Telemetry Systems

End-to-end health monitoring with real-time telemetry visualization and alerting.

Validation & Operational Experience

Kepler subsystems have been validated through deployment in operational environments across national and strategic programs.

Our focus remains on integration readiness and operational consistency.

Multiple components have achieved TRL-8 and TRL-9 through

Flight validation
Ground operational use
Long-duration deployment
TRL 8–9 Flight & Operationally Validated

Engineering Principles

Modular System Architecture

Plug-and-play subsystem blocks that reduce integration time and risk.

Integration-First Design

Every interface, connector, and protocol chosen for mission compatibility.

Performance-Driven Hardware

Specifications derived from real mission requirements, not lab benchmarks.

International Standards Compliance

Compatible with CCSDS, ECSS, and other international mission standards.

We design subsystems to reduce integration complexity and accelerate deployment timelines for satellite manufacturers and mission operators.