Technology

1gSpace vehicles are engineered for sustained 1 g acceleration to maintain Earth-equivalent gravity while executing deep-space trajectories. This operating regime minimizes deconditioning, simplifies crew biomechanics, and yields efficient point-to-point transfer profiles within mission Δv and power budgets.

Crewed platforms such as ISV Proxima and ISV Innes employ modular habitats designed for multi-year service. Subsystems include closed-loop ECLSS for air and water recovery, graded-density radiation protection, and adaptive environmental controls. Mission facilities integrate research labs, next-generation medical capability, recreation zones, and in-situ manufacturing via additive processes for tools and spares.

Communication architectures combine precision timing with optical deep-space links for high-integrity data return. Robotic free-flyers and surface/structure manipulators support external inspection, maintenance, and resource handling. Thermal management relies on high-emissivity radiators with engineered heat transport paths; where thermodynamically admissible, waste-heat scavenging augments shipboard power, with rejection sized to worst-case loads.

Operational oversight is provided by AURAI, a redundant autonomous control system that allocates propulsion and power, schedules resources, mitigates debris and micrometeoroid risk, and governs environmental controls. Predictive analytics and health-management models enforce margins, while real-time monitoring safeguards flight-critical functions across both crewed and unmanned assets.

DCMCAAFR Reactors

The Dual-Core Magnetically Confined Antiproton-Augmented Fusion Reactor (DCMCAAFR) family provides ship power and continuous-thrust capability for deep-space operations. Primary energy is derived from aneutronic p–B¹¹ fusion in dual confinement volumes; antiproton augmentation is applied under controlled conditions to shape ignition dynamics and stabilize burn. Metallic-hydrogen preconditioning is utilized for thermal input and plasma staging.

Full-scale DCMCAAFR installations on large crewed vehicles support sustained 1 g profiles, with magnetic-nozzle exhaust and vectored fields for precise attitude-coupled thrust. The dual-core topology enhances stability, affords graceful-degradation pathways, and enables concurrent power production and propulsion. Compact DCMCAAFR variants, as flown on ACEP, scale the architecture for autonomous deep-space reconnaissance while preserving high specific-impulse operation and robust energy conversion.