ENGINEERING CONCEPT / FLOW STAGE 03

Converging intake throat

The throat is the proposed physical interface between a very large capture envelope and the machinery housed in the spacecraft.

HYPOTHETICAL ARCHITECTURE · PERFORMANCE NOT VALIDATED
01 / THE SYSTEM'S ROLE

Turning a broad field into a controlled passage

The throat is the proposed physical interface between a very large capture envelope and the machinery housed in the spacecraft.

02 / SCIENCE WE CAN DISTINGUISH

Known effects vs. proposed extrapolation

Converging nozzles, flow conditioning and differential pressure are well understood for ordinary fluids and plasmas under stated conditions. They cannot simply be applied to unknown dark matter.

03 / THE SOURCE PROPOSAL

What the working reports suggest

The notes quote an approximately 1.2 km intake throat; alignment vanes, vortex stabilizers and field gradients are proposed to guide the substrate into the magnetic section. Their effects depend entirely on a validated coupling model.

04 / PHYSICAL HANDOFFS

How material or energy would move

  1. Receive particles from a much larger projected collection cross-section.
  2. Condition momentum and angular distribution to avoid mechanical loading.
  3. Deliver a measurable flux, with mass and energy accounted for, to the solenoid.
05 / UNRESOLVED CONDITION

The engineering uncertainty

A funnel-shaped drawing does not establish that a hypothetical dark medium responds to a physical wall or magnetic field. The source of convergence work and momentum has not been computed.

06 / FALSIFIABLE NEXT STEP

What a rigorous test needs

Measure incoming and outgoing momentum distributions, losses and backreaction through a testable interaction model; compare with a no-field control.

Editorial source track: Project integration notes; R02 — EIT Scoop Field. Report bodies are internal working documents, not independently reviewed physics.

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