OPEN SCHEMATIC ↗
FLOW STAGE 03 / CONCEPT DRAWING
Physical collection intake throat
The spacecraft-side entry aperture funnels already-directed substrate flow into controlled magnetic transport hardware.
Study components and limitations →Projected EIT collection field
The forward capture concept proposes a field thousands of kilometers across that guides extremely dilute, hypothetical dark-substrate excitations toward a smaller throat.
USER-SUPPLIED CONCEPT DRAWING · NOT VALIDATED ENGINEERING
01 / THE PRINCIPLE
What this assembly is supposed to do
EIT is a measured change in optical absorption and dispersion in suitable prepared media. The proposed ramscoop extrapolates this effect to a macroscopic vacuum environment and speculates that phase gradients and orbital-angular-momentum-like modes could provide a collecting force.
02 / CONNECTIONS AND BOUNDARIESHow it fits the engine
Interfaces to the intake throat, field emitter power, real-time density estimation and attitude pointing. A vacuum-scale EIT collecting force has not been demonstrated.
OPEN VALIDATION QUESTION
What measurable coupling, interaction cross-section, group velocity and power expenditure would be needed to capture the proposed substrate?
NEXT / CONNECTED HARDWARE
See the eight stages ↗Trace the interfaces.
OPEN SCHEMATIC ↗
OPEN SCHEMATIC ↗
SUPPORT / CONCEPT DRAWING
External beamed-power capture and distribution
Conceptual spacecraft power intake, rectenna or optical receiver, and distribution to high-field engine stages.
Study components and limitations →
OPEN SCHEMATIC ↗
SUPPORT / CONCEPT DRAWING
Star trackers, interferometry and navigation sensing
Precision position and attitude sensing across a hypothetical high-speed transit envelope.
Study components and limitations →THE JOURNEY STARTS WITH A QUESTION
Launch the simulator ↗Ready to see the flow?
Enter the interactive lab and explore the eight proposed stages.