The spacecraft-side entry aperture funnels already-directed substrate flow into controlled magnetic transport hardware.
The throat is drawn as a large, converging passage with flow alignment and field-boundary management. In the proposal it must handle injected wave packets without losing phase coherence or overwhelming the structure with drag.
02 / CONNECTIONS AND BOUNDARIESMust connect the projected scoop to the ~600 m solenoid. The physical mechanism responsible for collecting and steering hypothetical massive photons is not established.
How much momentum and energy arrive at the throat, and how can entry stability be proven under a range of ambient densities?
OPEN SCHEMATIC ↗
The forward capture concept proposes a field thousands of kilometers across that guides extremely dilute, hypothetical dark-substrate excitations toward a smaller throat.
Study components and limitations →
OPEN SCHEMATIC ↗
The proposed approximately 600 m magnetic transport section seeks to shape trajectories and manage intake drag.
Study components and limitations →
OPEN SCHEMATIC ↗
A forward impact-protection concept combining sacrificial material, cryogenic layers, repair circulation and magnetic interfaces.
Study components and limitations →Enter the interactive lab and explore the eight proposed stages.
Rule-based guide. No experimental claims or AI model calls.
