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 →Fishback superconducting solenoid
The proposed approximately 600 m magnetic transport section seeks to shape trajectories and manage intake drag.
USER-SUPPLIED CONCEPT DRAWING · NOT VALIDATED ENGINEERING
01 / THE PRINCIPLE
What this assembly is supposed to do
Concentric superconducting coils and feedback control form a tapered transport channel. The source invokes Weber/Machian relational interactions to hypothesize drag reduction, but the assertion of drag cancellation is not demonstrated.
02 / CONNECTIONS AND BOUNDARIESHow it fits the engine
The magnetic field and drag-cancellation claims require external verification. Any practical intake must conserve total momentum even if local forces are redistributed.
OPEN VALIDATION QUESTION
What field strengths, supports, cryogenic loads and measurable force balances would be required without assuming zero drag?
NEXT / CONNECTED HARDWARE
See the eight stages ↗Trace the interfaces.
OPEN SCHEMATIC ↗
OPEN SCHEMATIC ↗
FLOW STAGE 05 / CONCEPT DRAWING
900 m staged magnetic compression
A sequential electromagnetic stage intended to increase the density of an incoming hypothetical medium before storage.
Study components and limitations →
OPEN SCHEMATIC ↗
SUPPORT / CONCEPT DRAWING
Cryogenic systems and heat rejection
A distributed thermal-control study for superconducting windings, cold photon storage, shielding and power electronics.
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.