Heavy
Lift.

Concept design for a low-cost, one-way supply drop glider — maximizing payload fraction using passive aerodynamics and disposable materials.
Concept / Prototyping  |  Aerodynamics  |  Humanitarian Aid

The Concept.

Most aerial supply systems are expensive, recoverable, and complex. This concept inverts the model: design a glider that is meant to be used once, built from reinforced cardboard and foam, and capable of delivering meaningful payload mass from altitude with no active control system.

The design challenge is aerodynamic — maximizing lift-to-drag ratio while minimizing structural weight in materials that are cheap enough to treat as disposable. Passive control surfaces keep the system simple and manufacturable at scale.

Primary Structure

Reinforced Cardboard

Secondary

Foam Core

Control

Passive Surfaces

Design Goal

Max Payload Fraction

Application

Humanitarian Aid Drop

Design Specs.

Wing Profile High-lift, low-speed cambered
Payload Fraction Maximized — airframe weight minimized
Control System Fixed passive control surfaces
Materials Reinforced cardboard, foam, minimal fasteners
Unit Cost Target Sub-$10 at scale
Recovery None — single use

Design Decisions.

01
Passive-Only Control No servos, no actuators, no electronics. Fixed dihedral and swept geometry provide inherent roll stability. Eliminates the cost, weight, and failure modes of active control — acceptable for a supply drop that doesn't need precision targeting.
02
Cardboard + Foam Composite Corrugated cardboard provides axial stiffness at low weight. Foam core adds impact resistance and prevents buckling in the wing sections. Both materials are available globally, foldable for compact storage, and non-hazardous.
03
High-Lift Wing Profile Cambered low-speed airfoil geometry maximizes lift coefficient at the low Reynolds numbers typical of lightweight gliders descending at walking speeds. Prioritizes gentle descent angle over glide efficiency.

The Premise.

The most effective humanitarian delivery system is one that can be manufactured anywhere, deployed from a standard cargo aircraft, and doesn't need to be retrieved. The engineering challenge here is not complexity — it's radical simplicity. Reducing a flying vehicle to its absolute minimum without losing the ability to carry mass safely to ground.

Aerodynamics Passive Control Structural Design Low-Cost Manufacturing Humanitarian Aid Concept / Prototyping