Development

Skyvine is an architectural hypothesis and a research program, not a finished aircraft. Early work does not attempt a mile-scale delivery demonstration.

1. 01

   Lifting-module viability

   Lift per kilowatt, lift per installed pound, controllability, vibration, and counter-rotation.

2. 02

   Electrical viability

   High-voltage DC transmission, lightweight conductors, conversion, insulation, fault isolation, and attachments.

3. 03

   Tether viability

   Mass, stiffness range, fatigue, torsion, drag, coil formation, kinking, and entanglement.

4. 04

   Collective-flight viability

   Short multi-module formations in controlled wind: gust response, oscillation, local coordination.

5. 05

   Payload-handling viability

   Sliding structural line, base winch plus distal capstan, and whole-tether movement.

6. 06

   Range expansion

   Extend successful configurations into wind-supported middle spans and terminal-drone operations.

Principal risks—aerodynamics, tether drag, gust stability, electrical protection, fatigue, regulation, and overall economic margin—are significant, but they are separable and experimentally measurable.