Mechanical feasibility - 26 May 2026
The current optics fit the box, but they are not fabrication-ready.
EmberScope applies the same mechanical screen to the spherical, conic, and starter-freeform mirror candidates: package reserve, detector fit, clipping, manufacturability, tolerance path, and field-service constraints.
Mechanical screen
A candidate has to be mountable, sealed, cooled, cleaned, and aligned before optical performance matters.
Evidence boundary
This is a candidate evaluation, not a CAD release.
The screen uses the current review-package parameters, prescriptions, and ray-trace metrics. The prescription still lacks a final LWIR window, filter, stop, baffles, detector carrier, alignment datums, and tolerance model.
The useful result is narrower than a build approval: all three candidates are compact enough to carry forward, while none should be sent for fabrication until clipping, freeform limits, and tolerance acceptance are built into the next optical iteration.
Candidate disposition
The simplest mirrors are easier to build; the freeform branch is the optical leader but carries the highest mechanical risk.
| Candidate | Package result | Main risk | Disposition |
|---|---|---|---|
| Spherical | Historical POC screen: 65.5 mm span, 0.324 kg proxy, detector sanity pass. | Edge throughput falls to 0.38 and edge RMS spot is 12803 um. | Mechanically plausible bench-surrogate only. |
| Conic | Historical POC screen: 65.5 mm span, 0.324 kg proxy, detector sanity pass. | Same 0.38 edge throughput, with 12491 um edge RMS spot. | Keep as the low-complexity manufacturing comparator. |
| Starter freeform | Current source-spec package: 72.0 mm span, 0.664 kg proxy, detector sanity pass. | M2 and M3 freeform departures reach 4.6 mm and 9.1 mm; edge throughput is still 0.38. | Current optical leader, but not quote-ready. |
Cross-candidate findings
The package margin is real, but final usability is still dominated by clearance, baffles, and tolerances.
Package reserve
All three optical cores fit well inside the 150 mm cube and leave room for housing, window cell, baffles, electronics, and service access.
Detector bay
All three candidates pass the focal-plane sanity check, so the detector remains mechanically plausible at this review level.
Field clipping
All three candidates need another optical/mechanical iteration because the 1.5 deg edge field only retains 38 percent aperture-valid rays.
Manufacturing risk
The spherical and conic variants are easier to quote, while the starter-freeform surface departures need manufacturability limits and supplier review.
Missing hardware
The current prescriptions do not yet include the window cell, blackened baffles, detector focus mechanism, mirror-cell datums, or thermal straps.
Build decision
Keep all three variants in the trade, but delay fabrication until edge coverage, tolerances, and mounting datums are explicit.
Next iteration rules
The next optical pass should include the mechanical constraints directly in the merit function.
Preserve at least 35 mm side reserve around the optical core, hold the optical-core mass proxy below 0.6 kg unless performance justifies otherwise, and restore edge-field aperture-valid fraction to at least 0.80 before calling any branch prototype-ready.
Export mirror datums, keep-out zones, window/filter thickness, detector carrier depth, baffle envelope, stop placement, and tolerance limits with each prescription so the mechanical review is no longer a separate late-stage filter.