Companion to:
Scope. This document covers only the wing's own power system: how the wing feeds itself, how much power it makes and stores, how it steps down when short, and, in detail, how every part is built into or onto the wing. It is the design authority for the contactless charging across the bearing that Build Guide sec 6.6 points to. Changelog, version history, and decision notes for this guide live in the central Changelog. Terms used here.
| Term | Plain meaning |
|---|---|
| Feather | The wing turned edge-on to the wind, making no force. Its safe resting state |
| Trim tab | The small flap on the tail. The only powered moving surface in the rig |
| Pod | The sealed electronics box at the wing root, on the turning side |
| Split transformer | Two facing coils that pass power by magnetism across an air gap, with nothing touching |
| Slip ring | The usual way to get power across a turning joint, by sliding contacts. Deliberately not used here |
| Ideal diode | A one-way electronic valve, so a dead battery drops off the bus instead of dragging it down |
| Awareness rail | The 3.3 V supply feeding only the computer, sensors, and radio |
| BMS | Battery management system. The little board that protects a battery pack |
| Compliance link | A spring-loaded section in the tab pushrod. A wind-load fuse: it lets strong wind push the tab straight whatever the actuator is doing, so feather never depends on power (Trim Actuator Guide v9.6 sec 6) |
| MPPT | Maximum power point tracking. A small charge controller that pulls the most it can from a solar cell as the light changes |
| RS485 | A rugged two-wire way of sending serial data. Immune to electrical noise |
| CAN | A two-wire data bus with error checking built in. What the Thomson actuator speaks |
The wing turns on a bearing to follow the wind. Nothing electrical crosses that turning joint by wire, a deliberate choice, so there is no slip ring to wear out. Instead the wing is its own small power island: it makes power, stores it, and uses it, all on the turning side. The only things that cross the joint are magnetism from a split transformer that can charge the wing from the hull without touching, and a short-range radio for commands and readings.
Its only real load is the small actuator that drives the tail's trim tab, plus a wind sensor, an angle sensor, a small computer, and the radio. The tab is what keeps that load small. The tail flies itself, and the actuator only positions a small flap against a light spring, so holding a trim setting draws essentially nothing. On a good day a small solar panel covers all of it.
The wing never loses the ability to trim itself for lack of power. And if it ever does, it simply feathers, turns edge-on to the wind, the safe resting state, and drifts, costing nothing but a little speed. Three independent ways to keep it powered, so no single failure takes away wing control:
One thing to keep clear: safety never depends on any of this. Feathering needs no power: the compliance link in the tab pushrod is a wind-load fuse that lets strong wind push the tab straight whatever the actuator is doing, and the light hinge spring centers it (Trim Actuator Guide v9.6 sec 6). The power system only buys performance, meaning the ability to keep actively working the wing, and awareness.
The whole wing runs on two rails, and everything in this document hangs off one of them.
| Rail | What it is | What lives on it |
|---|---|---|
| 24 V bus | Both batteries (25.6 V nominal LiFePO4) joined through one-way ideal diodes, so either feeds the bus and a dead one drops out | Tab actuator, battery chargers, the receiving coupler's output |
| 3.3 V awareness rail | Stepped down from the 24 V bus. Falls back automatically to the backup cell when the bus is dead | Computer, wind sensor, angle sensor, radio |
Charging sources all land on the 24 V side. The solar cells feed it through two small MPPT charge controllers, one per face. The contactless coupler, a small 24 V inductive coil pair, feeds the wing charge controller like a panel (sec 4.2). The backup cell is a 3.6 volt lithium primary. It feeds only the 3.3 volt awareness rail, through its own regulator and diode, switching in by itself when both batteries are gone. Nothing about the backup cell involves the actuator. It cannot move the tab and never needs to, because feather is the compliance link's job, not power's.
| Part | What it does | Roughly |
|---|---|---|
| Solar cells, both faces | Make power in daylight | 4 sq ft total, about 2 lb |
| Battery 1 and Battery 2 | Store power. Either one runs everything | 24 V (25.6 V nominal) 6 Ah LiFePO4, about 150 Wh and 2.9 lb each, as bought |
| Backup cell | Keeps sensors and radio alive if both batteries are flat | OmniCel ER34615 lithium D-cell with leads, about 0.25 lb |
| Receiving coupler (turning half) | Receives charge from the hull, with no contact | Receiving coil of a 24 V inductive coil pair bought on Amazon 2026-09-15; part number and rating to be logged at the next mail audit. Light; weight to be measured |
| Pod electronics | Computer, radio, angle sensor, charge controllers, watchdog | Existing pod |
| Tab actuator | Drives the tail's trim tab. Lives in the sealed boom root fairing, 47 in up, fed by one wiring conduit in the trailing edge. The only real power user | Thomson Electrak MD, about 2.4 lb. Trim Actuator Guide v9.6 sec 2 |
| Wind sensor | Reads the wind at the wing tip. The cross-check for the primary unit on the instrument post | Calypso CMI1017 ultrasonic (RS485), on a short arm ahead of the nose at the tip |
Total added weight at the wing root is about 9 to 10 lb, all of it low. Both battery packs ride in the external nose locker on the root leading edge (Wing Construction Guide v9.6 Stage 10), where the same weight does balance work ahead of the pivot. Batteries the wing carries anyway replace lead. The actuator rides at the boom root and is carried in the same moment budget: about 2.4 lb for the Thomson MD.
Two square feet on each face, both faces, for 4 sq ft in total. Why both faces. The wing is a tall vertical shape that swings to point into the wind, so a panel is never aimed straight at the sun. Cells go on both faces and the system simply draws from whichever side is brighter at the moment. They are built flush into the skin (sec 8.2) so there is nothing sticking up to peel off. Rough daily output:
| Where | Output |
|---|---|
| Tropics | About 45 Wh per day |
| Mid-latitudes | About 35 Wh per day |
| Southern Ocean, worst and cloudy | About 10 Wh per day |
This is a bought part, not a project. The part: a 24 V inductive coil pair bought on Amazon 2026-09-15, part number and rating to be logged at the next mail audit. About $45. One coil is powered on the fixed side, the other receives on the turning side, and power passes by magnetism across a small air gap with nothing touching. The rating is not known yet, so the check is written down here. The wing itself uses about 20 Wh a day fully active (sec 5), which any coupler of this class refills in a few hours whenever hull power is healthy. The load that decides the part is the heater pads: the pod needs about 20 W if both pads run from the coupler, and a few watts otherwise. So either the coupler carries the pad load, or the pads run from the pod packs (sec 8.3). Measure it at the sec 10 coupler test. The receiving coil feeds the wing charge controller as if it were a solar panel. History, one line: the Phoenix Contact NearFi 200 pair (50 W, about $650) was the specified coupler through v9.6 revision 1. It, its M12 cordsets and its G10 standoffs are deleted, 60x oversized for this wing. Do not re-propose it. This lets the hull charge the wing without a slip ring. It only works when the hull's main power is alive; when the hull is dead the wing runs on its own solar and batteries instead. Mounting is in sec 8.5.
Two batteries, 25.6 volt 6 amp-hour LiFePO4, about 150 watt-hours each, on the aft shelf of the external nose locker at the wing root. Mounting in sec 8.3. Either one alone runs the entire wing, so losing one is not a crisis. The sizing requirement, stated plainly: ride out a two-week total-overcast storm sequence on ONE battery, in reduced mode, with solar cut in half. One 150 Wh battery covers about 16 days of that case, so the pair carries the requirement with a whole battery of redundancy on top.
The Southern Ocean is the hard case: short on sun, long on wind. There is a silver lining. Strong wind means the wing barely needs active damping there, so it uses very little power. Holding trim draws essentially nothing with the tab; only moving it costs anything. Per-device design values:
| Device | Average draw |
|---|---|
| Computer and sensors | ~0.15 W |
| Wind sensor | 0.2 W |
| Radio beacon | 0.05 W |
| Actuator movement, full active | 0.4 W |
The daily balance, with solar making about 10 Wh per day:
| Wing mode | Uses per day | Result on solar alone |
|---|---|---|
| Full active, all damping on | About 20 Wh | Short each day; battery makes up the difference |
| Reduced, light damping | About 14 Wh | Small shortfall; battery covers it |
| Coarse, damping off but still trimming | About 7 Wh | Roughly break-even on solar alone |
| Feathered, resting | About 2.5 Wh | Solar makes several times what it needs |
The last line is the important one. Feathered, the wing makes far more than it uses, even in the worst light. So low sun can never permanently drain it. If it runs low it drops toward feather, refills its batteries, and comes back. The batteries are only there to buy active-sailing time through dark patches.
The wing watches its own battery level and steps itself down, the same way the whole boat does.
| Battery level | What the wing does |
|---|---|
| High | Full active trim and damping, normal readings sent |
| Medium | Lighter damping, slower sensor checks, beacon-only readings |
| Low | Damping off. The wing hunts a little but still trims and steers; computer mostly asleep |
| Critical | Feather and sleep. Wake now and then. Drift east, which is progress |
Turning damping off when low is safe and nearly free. Damping is just software smoothing. It is not what keeps the wing safe; the compliance link does that. And shedding trim entirely is safe: an unpowered tab holds its last position in light wind, where it cannot hurt anything, and in strong wind the compliance link lets it straighten, which is a feathered wing. With damping off the wing wanders a few degrees around its heading and loses a little speed. It still trims and steers. The Southern Ocean is windy, and damping is barely needed in wind. So you give up almost nothing by shedding it right where you are shortest on sun.
A link drop is a comms failure, not a wing failure. The wing still has its own wind sensor, computer, and batteries. Going straight to feather on a 30-second dropout would stop the boat many times a voyage. So feather is the END of the ladder, not the first step.
| Outage length | Response |
|---|---|
| Under 10 minutes | Hold the last commanded trim. Most dropouts are seconds |
| 10 minutes to 2 hours | Self-trim on the wing's own wind sensor at a reduced setting, about 60 to 70 percent of the last commanded angle |
| Over 2 hours, or wing battery below reserve, or wind above the storm threshold | Feather, on the wing's own power ladder |
How the middle rung works: it is the same trick a wind-vane self-steering gear uses. Hold a fixed angle to the measured wind, without knowing where the boat is going. The wing cannot overload anything because it is trimming to measured wind, and the boat keeps making way. Bench test: power the wing up, kill the radio, and watch it walk the ladder on its own clock. Folds into the section 10 tests.
Use thin flexible back-contact cells, the kind with no metal lines on the top face. The rule is simple: the cells become part of the skin, flush, with no edge for the wind to grab.
Now each cell is captured on every side and sits flush. A 60 kt wind has nothing to lift. Keep the cells off the front 6 to 8 in of the wing, which takes the wave slams.
Lay TWO EXTRA PLIES of glass under each cell pocket during the skin layup, and keep a white-painted border around each pocket. Never let dark encapsulation run past the cell edge. Why. A solar cell absorbs 90 to 95 percent of the sun that hits it, against 20 to 25 percent for the white paint. That is four times the heat into the same surface. In windless tropical sun, a dark cell over H80 foam approaches the foam's softening range: H80 is good to about 158 F continuous, roughly 176 F short-term. Glass spreads heat about 5 times better than epoxy, and costs a scrap of cloth. GATE: soak one cell-on-coupon sample at 176 F and look for print-through or softening before committing the wing. Only if the coupon fails, add 0.005 in adhesive-backed COPPER foil under each pocket.
Simply OVERPAINT the film's lap border with the same white one-part Rust-Oleum Marine Topside the wing already wears. Twenty minutes, and it is the 90 percent fix. A routed rebate for the film edge was considered and skipped. The failure it guards against, the lap edge lifting under UV and salt, costs one cell string, and the wing's solar is about 10 Wh/day of backup against a 50 W hull feed. It is not a boat problem.
If you prefer, the cells can instead be laid between the outer two glass layers during the skin layup, then covered with a clear coat. Same result: cells inside the skin, nothing on top to peel.
Each battery is a 24 V (25.6 V nominal) 6 Ah LiFePO4 pack, about 150 Wh, 2.9 lb as bought. Confirm the pack dimensions before the locker plug is cut (Wing Construction Guide v9.6 Stage 10). The packs get no boxes of their own. Both ride on the aft shelf of the external nose locker on the root leading edge. The Wing Construction Guide v9.6 (Stage 10) owns the locker build: saddle, through-bolts, gasketed lid, drains, and vent. This guide owns the packs and their wiring.
LiFePO4 batteries must not be charged below freezing. Below 32 F the lithium plates onto the anode instead of going in, and the damage is permanent. Discharge is fine to -4 F. Fitted now, not deferred to lake testing that cannot produce Southern Ocean cold: a hard charge inhibit at 35 F, independent of software.
Thermostated heater pads under each pack are fitted, with one hard constraint written here so it is never violated. The pod heaters STAY: the main-bank heaters were deleted because the sea holds that pack above freezing, but these pod packs sit aloft in the nose locker and follow air temperature. Do not re-propose deleting them. Parts: two 24 V 10 W silicone pads, 2 x 2 in (bought), with a pair of 24 V XH-W3001 thermostats, one per pad. A 10 W pad running continuously is 240 Wh/day, against a wing budget of about 20 Wh/day and about 10 Wh/day of solar. So: THE PADS RUN ONLY ON HULL POWER THROUGH THE COUPLER. On wing power a 10 W pad would empty a 150 Wh pack in well under a day. Cold-charge heating is a hull-powered function, never a wing-battery one. With the hull dead, the packs simply wait for sun-warmth, protected by the inhibit. One check to make: the coupler's rating is not logged yet (sec 4.2), and two 10 W pads plus the pod's own few watts is about 20 W. The thermostats cycle the pads, so the average is lower, but confirm at the sec 10 coupler test that the pads warm the packs on the coupler alone. If they cannot, the choice is a bigger coupler or running the pads from the pod packs, which the rule above otherwise forbids; record the measured figure and put that choice to Mike. Nothing else in this guide changes.
One lithium primary D-cell: the OmniCel ER34615 with leads, 3.6 volt lithium thionyl chloride, about 19 amp-hours, with very long shelf life. In a sealed holder, potted, mounted anywhere dry in the pod. It feeds only the 3.3 volt awareness rail, through its own regulator and one-way diode, and switches in by itself when both batteries are gone. It keeps the computer, sensors, and radio beacon alive for about two weeks at beacon duty. The arithmetic: the sec 5 device table sums to about 0.4 W with everything awake (0.15 W computer and sensors, 0.2 W wind sensor, 0.05 W radio beacon). On the backup cell the pod is in its sleep ladder, computer and sensors duty-cycled to roughly half time, so the average draw is about 0.2 W. The cell holds about 68 Wh (3.6 V x 19 Ah), and 68 Wh / 0.2 W is about 340 hours, about 14 days. What it does not do, on purpose: it never powers the actuator. A single D-cell cannot source actuator current. It does not need to. Losing all trim power never puts the wing at risk: the compliance link is the fuse, and it feathers the wing in any wind that could hurt it. Mark the cell with the install date and replace it at the big pre-voyage refit.
Lithium thionyl chloride cells grow a film on the anode while sitting unloaded. That film is what gives them their shelf life, and it costs only a couple of percent of capacity a year. But it makes the FIRST current pulse sag, sometimes for seconds to minutes. If the beacon's transmit pulse drags the cell below the radio's brownout, the transmission fails until the film breaks down. The risk is neither lost capacity nor total failure. It is that first pulse. And the cell has no fat to give: about 68 Wh against the 0.2 W average duty-cycled draw (sec 8.4) is roughly two weeks, exactly the stated claim. The fix costs a resistor and a MOSFET: pull 10 to 50 mA for 30 seconds once a month, and log the voltage. The logged voltage IS the health trend.
Two bought coils and their leads. Nothing wound, nothing tuned. The part is the 24 V inductive coil pair of sec 4.2 (bought on Amazon 2026-09-15; part number and rating to be logged at the next mail audit): one transmitting coil with its small driver board on the fixed side, one receiving coil on the turning side.
Put surge protectors on both sides, and keep this circuit separate from the lightning bonding strap that already bridges the bearing, so a strike does not travel through the coils. The coil pair carries no weather rating of its own, so its driver board is conformal-coated and its lead exits potted. Both halves live in the most sheltered spot on the boat, inside the can under the labyrinth skirt.
A sealed housing at the wing root, on the turning side, holding:
The two battery packs ride forward in the nose locker (sec 8.3). The actuator does not live here; it is up in the boom root fairing at the end of the wiring run. Build rules:
The pod computer gets a wing-side hardware watchdog: the same Nano-plus-regulator recipe as the hull watchdogs. The pod software must pet the watchdog on schedule. If the petting stops, the watchdog power-cycles the pod computer's rail. Two build rules are pass/fail:
So a hung pod reboots itself. While it reboots, nothing drives the actuator: the tab holds its last position, and in strong wind the compliance link lets it straighten. A healthy reboot resumes sailing. Section 10 has the bench test that proves both rules.
| If this fails | What happens | Why it is OK |
|---|---|---|
| A solar cell tears or dies | Lose a little charging | Cells are flush and captured, so no debris reaches the trim parts. The transformer and batteries still charge and run the wing |
| All wing solar lost in a storm | No wing charging during the storm | In a storm the wing is feathered and barely using power. The batteries and the transformer cover it |
| The transformer or hull power fails | No charging from the hull | Wing solar and the batteries carry on |
| One battery or its board fails | Half the storage is gone | The other battery alone carries the design case: about 16 days of reduced-mode sailing through storm overcast |
| The trim wiring or the actuator fails | No active trim | The tab holds where it was. In strong wind the compliance link in the pushrod gives, the tab straightens, the tail streamlines, and the wing feathers. Light wind cannot hurt the rig |
| The pod computer hangs | The watchdog power-cycles its rail. The tab holds its last position while it reboots, then sailing resumes | The watchdog's pass element defaults ON and its action is a cycle, never a latch-off. So a dead watchdog cannot cut power, and a hung computer cannot stay hung |
| Both batteries flat and still no sun | No active trim | The wing is safe without power: the compliance link feathers it in any wind that matters, and it drifts east. The backup cell keeps sensors and radio alive so you still see its state |
| Backup cell also dead, or years old | If the batteries are flat too, the wing goes silent | Still safe: feather is the compliance link's job. The wing weathervanes edge-on and recharges on the next sun. Replace the cell at every refit so this stays theoretical |
| The whole pod goes dark | No active trim, no readings | The wing still feathers mechanically, the boat is safe, it just drifts until the sun returns |
The single most important point: losing wing power is never a safety failure. The wing's safe state, feathered, is set by the compliance link and the hinge spring, and needs no power. And it is also the state in which the wing makes the most surplus solar. Everything above only protects performance and awareness.
The two proof tests of the Trim Actuator Guide v9.6 sec 7, both mandatory, with the wing on the bench and again on the boat:
The old test (cut power, the tab springs straight) is deleted. With the link as the fuse, and with a self-locking actuator, it cannot pass and proves nothing.
After the component closure-verification battery and the high-wind buffet run (Build Guide sec 11.2; the build verifies watertight-at-any-angle by component flood and hose tests rather than a whole-boat inversion):
Cover and uncover the cells, and confirm both faces feed the batteries and the charge controllers behave.
| Item | Rough cost |
|---|---|
| Flexible back-contact solar cells, about 4 sq ft, plus clear encapsulation | $300 |
| Two 24 V 6 Ah LiFePO4 packs (about 150 Wh, 2.9 lb each) with their BMS boards, bought; locker shelf mounting hardware | $300 (estimate; the order sheet has the bought price) |
| OmniCel ER34615 backup D-cell with leads, and holder | $30 |
| 24 V inductive coil pair bought on Amazon 2026-09-15; part number and rating to be logged at the next mail audit | $45 |
| Pod watchdog (Nano, regulator, small parts, same recipe as the hull watchdogs) | $30 |
| Solar electronics option A: two 5 A MPPT boards, 8 to 28 V (bought), and two DG7512 ideal-diode boards (one bought, one to buy) | in the line below |
| Pod pack heaters: two 24 V 10 W silicone pads, 2 x 2 in (bought), and two 24 V XH-W3001 thermostats | see Bill of Materials v9.6 |
| Wing wiring conduit: 1/4 in OD sealed nylon tube, 100 ft (bought) | see Bill of Materials v9.6 |
| Trailing-edge cable: tinned 18/4 shielded, 50 ft, on the buy list (Amazon B0D9JV83HJ, tinned, shielded). The bare-copper roll goes back | $36.99 |
| Wiring, glands, conformal coat, and the solar electronics above | $220 |
| Total | $925 (rough; the Bill of Materials v9.6 and the order sheet carry the bought prices) |
Budget history and part substitutions are recorded in the central Changelog.