We are genuinely, unreservedly excited to share this. Not excited in the way that press releases get excited — excited in the way that happens when you've been working on something for a long time, the pieces come together in a way that surprises even you, and you realize the numbers actually hold up. That's where we are with the DragonSuit Apex research proposal, and we want to walk you through exactly what it contains and why it matters.
The problem nobody was solving
Wingsuit design has been stuck for thirty years. Not for lack of effort — for lack of methodology. The entire industry has iterated by feel: a practitioner sews fabric between their limbs, jumps out of a plane, survives if they're lucky, and adjusts the pattern. There has been no computational fluid dynamics applied to the full-suit geometry. No materials science. No physics-first design process.
The result is that the best commercial wingsuits today achieve a glide ratio of roughly 2.8–3.0:1 — meaning for every foot you drop, you travel about three feet forward. That number has barely moved in a decade. It sits there not because the physics are exhausted, but because nobody asked the physics the right question.
We asked the question. And then we looked at what four billion years of evolution had already figured out.
"Every technology in the DragonSuit traces directly to a biological mechanism that a real creature solved first — and solved better than anything we've engineered from scratch."
Five layers. Five biological solutions. One wing.
The DragonSuit Apex arm-wing and leg-wing panels incorporate five distinct functional layers, each of which addresses a specific aerodynamic failure mode that conventional wingsuits never touched.
What the numbers look like when it all comes together
The research proposal includes a full glide ratio projection — technology by technology — with published literature as the validation basis for each individual component. When we sum the contributions with a conservative 30% interaction discount applied, the projected L/D for the full Apex stack lands at 5.0–6.0:1. The best conventional suit today: 2.8–3.0:1.
That is a genuine 2× improvement in glide performance. Not a rounding error. Not a marketing multiplier. The CFD-based analysis that produces that number is documented in the proposal — every assumption is stated, every reference is cited, and every claim connects to a measurable physical mechanism validated somewhere in the scientific literature.
The safety implication is equally significant. A higher stall angle — extended here from 22° to ~28° by the tubercle geometry — directly translates to a lower minimum deployment altitude. Our design target: 51% reduction in minimum safe opening altitude versus best-in-class. In proximity wingsuit flying, that number can be the difference between a recoverable situation and one that isn't.
Why we're proposing a wind tunnel aerodynamics program
We're honest about what we have and what we don't. The projection is well-grounded in published science. What we don't yet have is instrumented experimental data confirming the projection for our specific geometry, at our specific Reynolds numbers, with all five layers integrated. That's exactly what a wind tunnel program with a university aerodynamics research facility would deliver.
| Configuration | What it tests | Key measurement |
|---|---|---|
| A — Isolated Arm-Wing Panel | 350 mm chord × 600 mm span panel, full five-layer stack, on a two-component force balance | CL, CD polars vs. NACA 4412 baseline; riblet Cf reduction |
| B — Full-Suit Mannequin | Rigid mannequin (5'11" / 150 lb reference pilot) with deployed arm and leg wings on a six-component sting balance | Full-suit L/D; body-wing interference effects; leg-wing contribution |
| C — Technology Isolation | Config A repeated with individual layers swapped out one at a time for baseline equivalents | Per-technology ΔL/D contribution matrix; direct comparison to projections |
The target deliverable beyond the data itself: a peer-reviewed manuscript submitted to the AIAA Journal or the Journal of Fluids and Structures. This research belongs in the scientific literature, and we intend to put it there.
The product line this research underpins
The wind tunnel program doesn't exist in a vacuum. It's the validation backbone for a four-SKU product line ranging from a $279 consumer entry suit (the Scout, with EVA foam ribs and a TPU tubercle strip) up to a $45K military specification suit (the Apex-M, adding helicoidal CFRP ballistic armor and MOLLE integration over the full aerodynamic stack). In between: the $10K–$18K Apex for elite pilots, and the $18K–$24K Apex-SAR for search and rescue.
The same composite stack — riblet film, auxetic panel, SMP skeleton — seeds three additional wearable platforms already in development: AquaSuit, GripSuit, and JumpSuit. The materials science is the platform. The wingsuit is the proof of concept.
On sharing this openly
We made a deliberate choice to publish this research without restriction. Our position: if someone reads this proposal, understands the physics well enough to build it, and makes something that flies — that would be among the greatest forms of validation we could receive. Ideas at this level want to exist in the world. We're here to make them happen first and build the organization that takes them to scale.
This proposal is the first document DragonWorx has published with the depth and rigor we believe the science deserves. It won't be the last.
Read the full research proposal
28 pages. 12 engineering drawings. Full technology stack. Proposed wind tunnel protocol. Complete reference list.
Download the PDF →About DragonWorx
DragonWorx Biomimetic Technologies applies aerospace materials science and biomimetics to wearable systems, aquatic platforms, and structural materials. Based in Richardson, Texas. Seed round in progress — $1.8M target. All inquiries: getdragons@dragonworx.bio