Low Earth Orbit
Integrated power, propulsion and spacecraft energy management for high-duty-cycle satellites, hosted payloads, servicing platforms and commercial stations.
TilghmanKraftwerkTILGHIESPACE
Pioneering power systems beyond Earth
Powering the cislunar economy.
TilghieSpace is developing the mission architecture for OMER‑III‑S: integrated power, propulsion, telemetry and autonomous energy management for low Earth orbit, cislunar space and future deep-space infrastructure.
Developmental mission architecture
01 / Thesis
Energy is the mission constraint
Space infrastructure cannot scale on yesterday's power density.
More available power means more capable payloads, faster electric propulsion, higher-bandwidth communications, stronger onboard computing and longer mission life. TilghieSpace is organized around that leverage point.
02 / Mission markets
From orbit to the Moon and beyond
Three operating domains. One integrated power thesis.
Each market is approached as an integrated system—generation, distribution, propulsion, communications, telemetry and thermal management—not as isolated hardware.
Cislunar Infrastructure
Future power architectures for communications and navigation relays, cargo tugs, lunar science platforms and sustained operations throughout Earth–Moon space.
Deep-Space Systems
Long-duration power and high-specific-impulse propulsion concepts intended to expand payload capability, mission endurance and operating range.
03 / Integrated architecture
Power is the system of systems
Generate. Distribute. Navigate. Move.
Generate
OMER‑III‑S is the proposed space derivative of the terrestrial OMER‑III research platform, designed around compact high-density power.
Distribute
Power management and distribution would connect generation, storage, payloads, avionics, thermal systems and propulsion as one controlled architecture.
Navigate
Telemetry, tracking and command, communications payloads and autonomous health management would provide the information layer for persistent operations.
Move
Fusion-electric propulsion research is intended to convert available electrical power into efficient, long-duration mobility for orbital and cislunar missions.
04 / Business plan
A staged route to revenue
Build valuable systems before the reactor flies.
The near-term business is not dependent on immediately fielding a fusion reactor in orbit. TilghieSpace can develop enabling power, telemetry, autonomy and integration capabilities that support conventional spacecraft first.
Engineering & integration
Mission power studies, spacecraft energy architecture, telemetry integration, power-management electronics and propulsion-system integration.
Flight hardware & demonstrations
Modular power-control units, autonomous monitoring, hosted technology demonstrations and high-power electric-propulsion packages.
Power and mobility infrastructure
OMER‑III‑S modules, orbital power platforms, cislunar transport systems and potential power-as-a-service mission models.
05 / Development sequence
Ground truth before flight
A credible path from terrestrial experiments to cislunar infrastructure.
1
Phase ITerrestrial validation
Retire OMER‑III physics and direct-conversion risks in ground-based experiments.
2
Phase IIOrbital demonstration
Demonstrate power management, telemetry and propulsion subsystems with conventional energy sources.
3
Phase IIIIntegrated space power
Advance a flight-qualified OMER‑III‑S architecture after terrestrial reactor validation.
4
Phase IVCislunar infrastructure
Scale toward persistent power and mobility services across the Earth–Moon economy.
06 / Engage
Space systems · strategic capital · mission partners