| Air Gap and Magnetic Pull Force |
| Direct metal-to-magnet contact | Air gap: approximately 0 mm | Highest reference force | Magnetic pull force is maximized when the magnetic circuit has minimal separation and a continuous ferromagnetic return path. | Measure axial pull force with a calibrated force gauge and a flat, clean steel target. |
| Thin textile or film cover | Air gap: approximately 0.2–0.5 mm | Usually high, but reduced | Even a small nonmagnetic layer can reduce force because magnetic field strength decreases rapidly as separation increases. | Test the complete product stack, including fabric, coating, adhesive, and liner thickness. |
| Thick padding or molded cover | Air gap: approximately 1–2 mm | Moderately reduced | Soft goods may remain closed during light loading, but the available pull margin can be substantially lower than the bare-magnet rating. | Repeat pull testing at the thinnest and thickest permitted material tolerances. |
| Large separation or misalignment | Air gap: greater than approximately 2 mm, or partial overlap | Potentially low | Magnetic coupling becomes sensitive to distance, offset, tilt, and the effective area of overlapping magnetic poles. | Test worst-case offset, angular misalignment, and maximum opening gap. |
| Important: Air-gap performance is geometry-dependent. Magnet diameter, thickness, pole arrangement, target material, target thickness, and surface area can change the measured force significantly. |
| Load Direction and Snap Retention |
| Normal pull or tensile load | Load acts directly away from the mating surface | Primary magnetic holding direction | Axial pull strength is the most common magnetic snap rating, but it should not be treated as the full product load capacity. | Record peak separation force using the final product construction, not only the loose component. |
| In-plane shear load | Load acts parallel to the mating surface | Depends on friction and alignment | Shear resistance is affected by the normal magnetic force, surface friction, enclosure material, and any mechanical interlock. | Use a horizontal shear test with controlled surface materials and a defined loading speed. |
| Combined pull and shear | Load has both perpendicular and parallel components | Lower margin than either load alone | Combined loading can reduce the force available in the most critical direction and may cause sliding before separation. | Test with the actual load angle and include repeated opening and closing cycles. |
| Peel load | One edge lifts while the opposite edge remains attached | Often the critical failure mode | Peel applies a rotating moment and concentrates separation at a small edge region, so the effective resistance may be far below the rated axial pull force. | Apply force at the expected opening edge and measure the initial peel force and peak force. |
| Useful Sizing Relationships |
| Required design resistance | Static or dynamic product load | Frequired = Fworking × S | Use a safety factor S appropriate to shock, vibration, material variation, user handling, and product life. | For noncritical closures, designers commonly begin with a safety factor of 2–3 and validate it through testing. |
| Shear resistance from friction | Magnet remains in contact with a mating surface | Fshear ≈ μN | μ is the coefficient of friction and N is the normal magnetic force. Covers and coatings can lower μ and therefore reduce shear capacity. | Measure friction using the actual fabric, polymer, coating, or metal contact surfaces. |
| Peel moment | Force is applied away from the closure center | M = F × d | M is the opening moment, F is the applied force, and d is the distance from the force line to the effective attachment area. | Reduce the lever arm, distribute the load across multiple snaps, or add a mechanical locating feature. |
| Product Design Considerations |
| Material stack-up | Fabric, foam, adhesive, coating, and cover are placed between mating parts | Can materially reduce force | Every nonmagnetic layer contributes to the air gap. Compression, seams, wrinkles, and manufacturing tolerances can produce local variation. | Specify maximum total stack thickness and verify the worst-case assembly. |
| Target material | Low-carbon steel, stainless steel, plated steel, or nonmagnetic material | Material-dependent | Ferromagnetic targets generally provide stronger coupling than nonmagnetic metals such as aluminum or copper. Stainless-steel magnetic behavior varies by grade and processing. | Test the exact target alloy, thickness, finish, and geometry used in production. |
| Alignment and overlap | Magnetic poles are centered and fully overlapped | Improved repeatability | Guides, pockets, or seam placement can prevent offset and reduce peel caused by edge loading. | Include tolerance limits for lateral offset, rotation, and closure position. |
| Repeated cycling | Frequent opening and closing over the product life | Requires durability validation | Magnet strength is generally stable, but covers, adhesives, stitching, coatings, and surrounding materials may wear or deform. | Perform cycle testing followed by pull, shear, and peel measurements. |
| Safety and handling | Small parts, sensitive electronics, or medical applications | Application-specific | Evaluate magnet retention, ingestion risk, magnetic-field compatibility, corrosion protection, and accidental detachment. | Document product-specific safety requirements and validate the complete assembly. |
| Practical Selection Checklist |
| 1 | Define the working loads in tensile, shear, and peel directions rather than relying only on an axial pull rating. |
| 2 | Measure the complete air gap, including fabric, foam, adhesive, coating, seam compression, and assembly tolerances. |
| 3 | Use the actual mating target and product materials during testing because magnetic performance is not transferable between all substrates. |
| 4 | Evaluate the worst-case misalignment and edge-loading condition, especially when the closure can be opened by peeling. |
| 5 | Apply an appropriate safety factor and confirm performance after environmental exposure and expected opening cycles. |