DragonWorx.Bio / Projects / Project A
PROJECT A โ€” ACTIVE DEVELOPMENT

DragonSuit

The first wingsuit designed from aerospace materials science first principles. Five-layer biomimetic composite stack. Four SKUs from consumer to military specification. Seed round in progress.

๐Ÿ‹ Humpback whale ๐Ÿฆˆ Shark skin ๐Ÿฆ… Peregrine falcon ๐Ÿฆ‘ Flying squid NACA 4412 SMP skeleton Auxetic panels
THE TECHNOLOGY

Physics first. Materials second. Suit last.

Every wingsuit before this was designed empirically โ€” a practitioner sewed fabric between their limbs and iterated if they survived. No computational fluid dynamics. No aerospace materials. No physics-first design methodology. The DragonSuit is what happens when you run the physics properly.

Technical Research Proposal
DragonSuit Apex โ€” Wind Tunnel Validation Program
28 pages ยท 12 engineering drawings ยท Five-layer composite stack, full instrumentation spec, TRL matrix, development timeline. Submitted to a university aerodynamics research program, May 2026.
Download PDF โ†’
BIOMIMETIC ยท TRL 4

๐Ÿ‹ Tubercle Leading Edges

Sinusoidal bumps from humpback whale pectoral fin geometry, applied to the arm-wing leading edge. Wavelength ~30% chord, amplitude ~5% chord. Delays stall from 22ยฐ to 28ยฐ angle of attack. Breaks the stall front into discrete spanwise cells via controlled micro-turbulence injection. Implemented as a precision TPU-molded strip on the Apex; silk-screened surface approximation on the Scout.

METAMATERIAL ยท TRL 4

๐Ÿ”ฌ Auxetic Panel โ€” Self-Cambering Wing

Negative Poisson's ratio re-entrant lattice embedded in the center wing panel. Under aerodynamic load, lateral expansion curves the chord into a higher-lift cambered profile โ€” the wing optimizes itself in response to the forces it experiences. Zero sensors, zero motors, zero feedback loop. Passive, load-triggered, geometry-based.

SMART MATERIAL ยท TRL 4

๐Ÿฆด Shape-Memory Polymer Skeleton

DiAPLEX SMP ribs profiled to NACA 4412 cross-section. Hold the wing geometry under aerodynamic load โ€” eliminating the fabric billow that degrades every conventional wingsuit's aerodynamic profile. Reset to flat at body heat (~37ยฐC). No mechanical parts. This single technology accounts for the largest share of the projected glide ratio improvement.

SURFACE SCIENCE ยท TRL 6

๐Ÿฆˆ Shark-Denticle Riblet Film

Laser-etched V-groove patterns confine quasi-streamwise vortices in the turbulent boundary layer, reducing skin friction drag 8โ€“10% in both air and water. Production-validated in Speedo Fastskin and Lufthansa Technik riblet programs. The highest TRL technology in the stack โ€” it works, it's been proven, and it applies to every other suit in the DragonWorx portfolio.

AERODYNAMIC ยท TRL 3

๐Ÿฆ… Peregrine Tip Slots

During a dive the falcon spreads primary feathers like fingers โ€” each slot converts tip vortex rotational energy into forward thrust vectors, reducing induced drag ~30%. The DragonSuit implementation uses the auxetic panel mechanism at the wingtip: load passively opens slot gaps without actuators. The single largest remaining untapped improvement in the design. Deep dive: The Feathers That Fold Drag into Thrust โ†’

STRUCTURAL ยท TRL 4โ€“5

๐Ÿ”€ Anisotropic Washout Weave

High-modulus fibers oriented spanwise with compliant fibers in the twist direction. Under load, the tip twists nose-down 3โ€“5ยฐ passively โ€” preventing tip stall through material stiffness gradient. Achieved entirely through the weave schedule. No added weight, no mechanical parts.

DragonSuit five-layer composite stack exploded diagram: (1) shark-skin micro-texture outer surface, (2) flex wing membrane, (3) adaptive morphing mesh, (4) energy weave layer, (5) base suit compression layer
Fig A.1 โ€” Five-layer composite stack. Each layer addresses a distinct physics problem: drag, shape, stiffness, energy, and fit.
Peregrine falcon slot-wing mechanism engineering sketch annotating primary feather slot opening, variable camber control, and turbulence-reducing air flow path โ€” the biological model for DragonSuit tip slot design
Fig A.2 โ€” Peregrine slot-wing sketch. Slots open to increase lift at low speed; air flow through slot reduces tip turbulence.
Leafspring joint system engineering sketch showing resilin core spring, carbon fiber composite structure, energy storage and return mechanism, and ankle flex assist โ€” the JumpSuit design foundation
Fig A.3 โ€” Leafspring joint system. Resilin + carbon fiber delivers 97% elastic energy return โ€” the foundation for the upcoming JumpSuit platform.
DragonSuit pilot launching into a glide over a deep canyon river at sunset โ€” demonstrating the consumer Apex SKU's open-air flight performance against a dramatic red-rock landscape
Consumer โ€” DragonSuit Apex

Canyon glide launch at dusk. The Apex's SMP rib skeleton holds NACA 4412 geometry under full aerodynamic load โ€” eliminating the wing billow that collapses conventional suits' glide performance at speed.

Military DragonSuit Apex-M operators conducting a high-altitude nighttime tactical insertion, gliding in formation over city lights โ€” demonstrating the military SKU's low-observable profile and MOLLE integration
Military โ€” DragonSuit Apex-M

High-altitude tactical insertion, formation flight. Apex-M adds helicoidal CFRP armor, NIJ-rated ballistic padding, and MOLLE attachment points over the full Apex aerodynamic stack.

DragonSuit Scout pilot flying with orange accent wing panels over glaciated alpine ridges โ€” the entry-level consumer SKU demonstrating stable 3.8โ€“4.5:1 glide ratio performance

DragonSuit Scout โ€” consumer entry SKU ($279โ€“$349). EVA foam ribs and TPU tubercle strip. 3.8โ€“4.5:1 glide ratio over alpine terrain.

PRODUCT LINE

Four SKUs. Three markets.

SKU Price Glide Ratio Min Altitude Key Differentiator Market
DragonSuit Scout $279โ€“$349 3.8โ€“4.5 : 1 ~120 ft EVA foam ribs + TPU tubercle strip Consumer / entry-level
DragonSuit Apex $10Kโ€“$18K 5.0โ€“6.0 : 1 ~90 ft Full 5-layer SMP stack Elite pilots
DragonSuit Apex-M $28Kโ€“$45K 5.0โ€“6.0 : 1 <90 ft Helicoidal CFRP + NIJ padding + MOLLE Military / SOF
DragonSuit Apex-SAR $18Kโ€“$24K 5.0โ€“6.0 : 1 ~90 ft Beacon integration + high-vis panels Search & Rescue / Gov

Glide ratio and altitude figures are design targets based on CFD simulation and published literature for individual component technologies. Wind tunnel validation planned with a university aerodynamics research program.

PLATFORM EXTENSIONS

The DragonSuit composite stack โ€” shark riblets, auxetic metamaterial, superhydrophobic surfaces โ€” directly seeds the next three suit platforms. The same materials science, different operating domains.

AquaSuit researcher diving alongside a sea turtle in a tropical coral reef โ€” the suit's boxfish-derived hull ridges and superhydrophobic plastron surface reducing hydrodynamic drag, with the shark-denticle riblet film shared directly from the DragonSuit material stack
AquaSuit โ€” Shark-denticle riblet film (TRL 6 in DragonSuit) transfers directly to aquatic drag reduction. Boxfish hull ridges add passive yaw stability. The same surface science, a different fluid medium.
GripSuit operator scaling a glass skyscraper face at night using gecko-inspired Van der Waals dry adhesion โ€” the nano-pillar array technology that pairs with the DragonSuit's auxetic panel geometry in a future multi-domain suit
GripSuit โ€” Hierarchical gecko nano-pillar adhesion. 10 N/cmยฒ dry, any surface. TRL 5 โ€” the highest-readiness upcoming platform after AquaSuit.

The physics, drawn.

Engineering drawings and performance diagrams extracted from the wind tunnel research proposal. All figures GPT-4o synthesis from design narrative unless noted.

Overview
DragonSuit three-view orthographic โ€” front, side, rear at scale 1:10
DS-01 Three-view orthographic โ€” wingspan 2,450 mm arm-to-arm (deployed). Reference pilot 5'11" / 150 lb. Scale 1:10. NACA 4412 profile visible along arm-wing chord in side view.
DragonSuit front-view orthographic โ€” arm wings at 45ยฐ deployment
DS-12 Front-view orthographic. Arm wings at ~45ยฐ deployment. Leg-wing panel geometry and torso junction seams visible. Scale 1:20.
Five-Layer Composite Stack
Five-layer composite stack exploded axonometric
DS-03 Five-layer stack, exploded axonometric. From outer surface inward: (1) shark-denticle riblet film, (2) flex wing membrane, (3) auxetic metamaterial mesh, (4) DiAPLEX SMP rib skeleton, (5) base compression layer. 30 cm ร— 30 cm panel section.
NACA 4412 arm-wing cross-section with five composite layer annotations
DS-02 NACA 4412 arm-wing cross-section, mid-span. Chord C = 350 mm. Max camber 14 mm (4.0%) at 40% chord. Max thickness 42 mm (12%). All five layers annotated at trailing-edge cutaway.
Shark-denticle riblet film surface texture at 500x scale
DS-08 Shark-denticle riblet film. Plan view at 500ร— scale โ€” V-groove riblets aligned with freestream direction. Groove depth g โ‰ˆ 20 ฮผm, spacing s โ‰ˆ 50 ฮผm. 8โ€“10% skin friction reduction. TRL 6, production-validated.
Auxetic metamaterial panel โ€” re-entrant hexagonal unit cell, loaded vs unloaded
DS-05 Auxetic metamaterial panel. Left: unloaded re-entrant hexagonal lattice (L = 10 mm, t = 1.5 mm, ฮธ = 120ยฐ). Right: loaded state overlay showing lateral expansion and chordwise cambering toward NACA 4412 target profile.
DiAPLEX SMP rib profile and two-state thermal cycle diagram
DS-09 DiAPLEX SMP rib profile. Chord C = 350 mm, NACA 4412 geometry. Two-state thermal cycle: glassy state below 37ยฐC (rigid, holds wing geometry); rubbery state at 37ยฐC (flexible, collapses to flat stow profile).
Biological Mechanism Technologies
Peregrine falcon tip slot โ€” right arm-wing tip zone, four slot gaps
DS-07 Peregrine tip slot โ€” right arm-wing tip zone (lateral 20% of span, ~300 mm). Four slot gaps shown unloaded (closed) and loaded (open, dashed). Slot width ~25 mm. Induced drag reduction target: ~30%.
Anisotropic washout weave โ€” passive tip twist under aerodynamic load
DS-06 Anisotropic washout weave. 40 cm ร— 40 cm panel section. Primary spanwise load-path fibers + compliant oblique twist fibers. Passive tip washout 3โ€“5ยฐ nose-down under aerodynamic load. No mechanical parts.
Performance Projections
Glide ratio comparison โ€” conventional baseline vs DragonSuit Apex design target
DS-10 Glide ratio comparison. Curve A: conventional baseline, peak L/D โ‰ˆ 2.8โ€“3.0 at ~12ยฐ AoA, stall at 22ยฐ. Curve B: DragonSuit Apex design target, peak L/D โ‰ˆ 5.5, stall delayed to 28ยฐ. CFD-based targets pending wind tunnel validation.
DragonSuit Scout simplified component diagram โ€” entry-level consumer SKU
DS-11 DragonSuit Scout component diagram โ€” entry-level consumer SKU ($279โ€“$349). EVA foam ribs replace DiAPLEX SMP. TPU tubercle strip retained at leading edge. Glide ratio target: 3.8โ€“4.5:1.
Engineering Drawing Package (DS-01 through DS-09)
DS-01 engineering drawing โ€” three-view orthographic
DS-01/12 Engineering drawing โ€” three-view orthographic. Scale 1:10. Front, side, rear with all critical dimensions labeled. Trailing-edge washout twist 6โ€“8ยฐ annotated in rear view.
DS-02 NACA 4412 arm-wing cross-section engineering drawing
DS-02 Engineering drawing โ€” NACA 4412 arm-wing cross-section. Chord C = 350 mm. All key dimensions, material annotations, and composite layer thicknesses.
DS-05 auxetic metamaterial panel engineering drawing
DS-05 Engineering drawing โ€” auxetic metamaterial panel. Nominal dimensions 40 cm ร— 60 cm. Unit cell geometry, loaded and unloaded state overlay, chordwise camber response annotation.
DS-06 anisotropic washout weave engineering drawing
DS-06 Engineering drawing โ€” anisotropic washout weave. Fiber architecture annotation, passive tip washout cross-section, 3โ€“5ยฐ nose-down rotation under aerodynamic load.
DS-07 peregrine tip slot engineering drawing
DS-07 Engineering drawing โ€” peregrine tip slot detail. Right arm-wing tip zone. Four slot gaps, unloaded (solid) and loaded (dashed). Vortex energy recovery diagram inset. Induced drag reduction target: ~30%.
DS-08 shark-denticle riblet film engineering drawing
DS-08 Engineering drawing โ€” shark-denticle riblet film. Plan view at 500ร— scale, Section A-A cross-section. Groove depth g โ‰ˆ 20 ฮผm, spacing s โ‰ˆ 50 ฮผm. TRL 6, production-validated in Speedo Fastskin and Lufthansa Technik programs.
DS-09 DiAPLEX SMP rib profile engineering drawing
DS-09 Engineering drawing โ€” DiAPLEX SMP rib profile and thermal state diagram. NACA 4412 cross-section at C = 350 mm. Two-state cycle: glassy (rigid, maintains geometry) and rubbery (flexible, collapses to stow profile at 37ยฐC).
DOWNLOADS & SUPPORTING DOCUMENTATION

Full documentation.

Technical proposals, research documentation, investor materials, and project planning tools. All documents are confidential โ€” not for redistribution without written consent.

Research Proposals
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DragonSuit Apex โ€” Wind Tunnel Research Proposal
PDF ยท 23 pages ยท 12 engineering drawings ยท Submitted to a university aerodynamics research program ยท May 2026 โ€” Five-layer biomimetic composite wingsuit: SMP ribs, auxetic panels, tubercle leading edge, shark riblets, peregrine tip slots. Projected 2ร— glide ratio improvement over best-in-class. Full wind tunnel test protocol and instrumentation spec.
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GripSuit โ€” From Gecko to Remora: Biomimetic Adhesion Stack Research Proposal
PDF ยท 15 pages ยท 7 engineering figures ยท Submitted to an advanced polymer research lab ยท May 2026 โ€” Four-mechanism adhesion stack (gecko vdW nano-pillars, clingfish compliant disc lip, remora lamellar spinules, DOPA-mimetic mussel chemistry) at human body-weight scale. Four research threads, full IP co-development framework.
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R&D Documentation
๐Ÿ“„
R&D White Paper โ€” Animal Superpowers at Human Scale
PDF ยท 18 pages ยท 14 biomimetic technologies, physics analysis, fabrication routes, TRL matrix across all active platforms.
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Project Planning
๐Ÿ“Š
DragonWorx Stage-Gate Project Plan
XLSX ยท May 2026 โ€” Structured stage-gate development roadmap covering all active platforms: DragonSuit, GripSuit, AquaSuit, JumpSuit, and ElectraSuit. Phase definitions, milestone gates, TRL advancement targets, resource allocation, and go/no-go decision criteria.
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Investor Materials
๐Ÿ“Š
DragonWorx Investor Deck 2026
PPTX ยท May 2026 ยท Seed round โ€” $1.8M target โ€” Company overview, full technology stack, five-platform roadmap, market opportunity by SKU, use of funds, and academic partnership pipeline.
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Contact: getdragons@dragonworx.bio