Lift Foils 200 Surf V2 Front Wing 200 hydrofoil front wing: 1,290 cm², 826 mm span, aspect ratio 5.40, with its closest equivalents from other brands within ±5% area and ±8% aspect ratio. Figures from Lift Foils's own published specifications.
Projected and flat area run 3–8% apart. A marked area is one whose brand does not state which it publishes, so a match inside the area tolerance may be comparing unlike figures.
| Brand | Wing | Area cm² | Δ area | Aspect ratio | Δ AR | Span mm | Band |
|---|---|---|---|---|---|---|---|
| Slingshot | One-Lock Ease 1250 | 1,250 | -3.1% | 5.30 | -1.9% | 817 | C1 Low aspect |
| Naish | Ultra Jet Front Wing Ultra Jet 1250 | 1,250 | -3.1% | 5.60 | +3.7% | 835 | C1 Low aspect |
| Armstrong | S1 (Step 1) S1 1250 | 1,250 | -3.1% | 5.70 | +5.6% | 848 | C1 Low aspect |
| Family | Surf V2 |
|---|---|
| Size | 200 |
| Area, cm² | 1,290 |
| Area basis | unknown |
| Span, mm | 826 |
| Chord, mm | — |
| Aspect ratio | 5.40 |
| Band | C1 Low aspect |
| Brand files it under | Surf / carve |
| Disciplines | prone, efoil, downwind, wing |
| Construction | standard modulus carbon |
| Model year | 2026 |
| Source | manufacturer |
The brand's published aspect ratio agrees with its own span and area (span² ÷ area) to within 5%, so the figure is confirmed.
See Lift Foils on the plot →Data current to August 2026. Fast Bobby is the researcher, never the reviewer: every figure above is the manufacturer's published claim, converted to comparable units, and nothing here is a riding impression.