P0 · PROTOTYPE FABRICATION RELEASE

SKY MECH / SKY MESH

Altitude is a resource you can pre-position.

SKY MECH P0 is a 6.0 m tethered helium prototype combining an external load harness, four nominal 100 W solar modules, serviceable sensor/relay pods, and two foldable visible-light observation gliders. Multiple nodes are intended to form a distributed SKY MESH coordinated by SHEEPDOG.

Several modest balloon mission units coordinate local UAV cells as a distributed coastal mesh.

6.0 mTethered helium envelope
16 goresRF-sealed fabrication pattern
4 × 100 WNominal removable solar modules
2 SKY SCOUTFoldable observation gliders

P0 prototype fabrication release

Not a render. A traceable prototype fabrication package.

The P0 release turns the SKY MECH node into supplier-reviewable geometry: 10 A3 drawing sheets, 9 DXF cutting files, 13 STEP geometry re-import checks and a 35-line BOM. It is intended for RFQ, first-article discussion and controlled tethered proof-of-concept work.

SKY MECH P0 complete balloon, solar carrier, payload pod and two scout gliders general arrangement.

Plate 01 · General arrangement

Complete balloon + scout kit

6.0 m tethered envelope, external load harness, serviceable pods, four nominal 100 W solar modules and two foldable observation gliders.

SKY MECH P0 envelope gore, RF seam and eight-leg external harness fabrication drawing.

Plate 02 · Envelope and harness

Cut patterns and load paths

Sixteen full-size gores, 20 mm RF seam allowance, interface reinforcement and an eight-leg external harness route.

SKY MECH P0 load ring, center mast, payload structure and solar carrier engineering drawing.

Plate 03 · Payload structure

Replaceable structure and power carrier

Ø1200 mm 6061-T6 ring geometry, Ø80 × 3 mm center mast, modular payload interfaces and four removable solar carriers.

SKY SCOUT P0 foldable visible-light observation glider airframe engineering drawing.

Plate 04 · SKY SCOUT airframe

Foldable visible-light observation glider

1.32 m span, 1.35 kg design mass, fold/deploy geometry, structural frame and avionics envelope. The flight release actuator remains outside P0.

PROTOTYPE FABRICATION RELEASE — CAPTIVE/TETHERED ENGINEERING POC · PERSONNEL LIFTING PROHIBITED · NON-WEAPONIZED OBSERVATION AND RELAY CONFIGURATION.

The node and the network

Small units. Shared mission state.

A SKY MECH unit provides a high vantage point, local communications, sensing, and a small reserve of unmanned capacity. SKY MESH emerges when several units share state, relay traffic, divide search space, and substitute for a lost node.

The valuable asset is not the balloon. It is the time, line of sight, and future options stored at altitude.

Several modest balloon mission units coordinate local UAV cells as a distributed coastal mesh.
Visual architecture: several low-cost balloon units, each supporting a small UAV cell and connected through a distributed mesh.

Tactical economics

Impose a response cost larger than the node.

The economic objective is a distributed node cheap enough to replace, but valuable enough to force an adversary to reveal, maneuver, launch, or expend a costlier interceptor.

Public cost anchorPublished figureHow to read it
NOAA radiosonde releaseAbout US$200A bare lower-bound anchor for a simple balloon and weather instrument—not a SKY MECH quote.
Baoqi SKY MECH planning envelopeUS$5k–25k per sensor/relay balloon prototype; US$30k–150k with six small UAVs and ground supportInternal concept range pending RFQ, recovery concept, payload, regulatory, and endurance trades.
FY2025 F-22A reimbursable rateUS$56,397 per flight hourOfficial U.S. reimbursement rate; not a full combat sortie cost.
FY2025 AIM-9X procurement averageAbout US$533k per missileUS$193.1M divided by 362 missiles; program average, not marginal engagement cost.

These are cost anchors, not apples-to-apples system quotes. The website will replace Baoqi planning envelopes with supplier RFQs and measured lifecycle cost as the program matures. Sources: NOAA/NWS and U.S. DoD FY2025 public documents.

Mission effects

Use stored altitude without building a giant aircraft.

SKY MECH high-altitude nodes coordinate layered aerial sensing and response over a protected area.

Layered airspace defense

Sense early. Assign the right layer. Preserve reserve.

SHEEPDOG classifies mission state, assigns sensing, relay, observation, and reserve roles, and replans after node or link loss.

High-altitude nodes, UAVs, and an unmanned surface vessel search a gridded maritime rescue area.

Search and rescue

Turn a wide area into a coordinated search matrix.

Partition the grid, overlap observations, fuse detections, and hand confirmed locations to USV or rescue teams.

Maritime incident confirmation

Verify the event before committing a larger asset.

Visible-light scout gliders and relay nodes support vessel identification, drifting-object observation, search-area confirmation and communications extension.

P0 excludes weapons, engagement guidance, certified flight release actuators and operational employment procedures.

Resilient sensing and relay

Recover the mission picture, not just the link.

When a unit degrades, SHEEPDOG evaluates which observations and connections matter most, reallocates another balloon or UAV, and records the consequence.

How SHEEPDOG governs the mesh

Every unit joins through a capability passport.

01 · DECLARE

Altitude, endurance, lift, sensing, links, UAV inventory, health.

02 · VALUE

Time-to-task, energy, replacement cost, reserve, future options.

03 · LEASE

Assign bounded sensing, relay, observation, or reserve roles.

04 · RECOVER

Release leases and reallocate after balloon, UAV, or link loss.

05 · PROVE

Replay the trigger, alternatives, authorization, outcome, and recovery.

Prototype boundary

Fabrication geometry is released. Flight evidence is still pending.

P0 provides supplier-reviewable structure, cutting geometry, interfaces, BOM and first-article checks. The next proof points remain physical weighing, envelope pressure testing, load-path proof testing, communications testing, controlled tethered operation, lawful airspace approval and platform integration.

Current boundary

SKY MECH P0 is a non-weaponized, captive/tethered engineering POC for fabrication and validation work. Personnel lifting is prohibited.

P0 geometry releasedControlled tethered POCPartner validation required

Research partnership

Help turn the cost envelope into measured evidence.

We are seeking high-altitude platform, communications, sensing, recovery, lawful test-range, maritime, and public-safety partners.