If you work with Camera Mirrors, you already know the stakes: thermal drift, coating stability, and delivery times that make or break projects. The Sitall Reflection Mirror, built in No. 1299 Mingxi Road,Beihu Science and Technology Developmeent Zone,Changchun,Jilin Province, leans into that reality with robotic CNC, ion-beam figuring, and old-school craft polishing where it still matters. Honestly, it’s a solid mix.
Three forces keep popping up: ultra-low expansion substrates, better asphere control, and coatings that survive field life. Sitall glass‑ceramic is hot because its CTE is close to zero, which helps maintain figure in satellites, machine vision lines, and even cinema rigs. Surprisingly, more teams request asymmetric aspheres to shrink optical trains—so production needs deterministic methods (IBF) plus metrology that doesn’t blink.
Materials: Sitall glass‑ceramic core (for low CTE), with Al, protected Ag, or dielectric HR coatings depending on band (VIS–NIR–MWIR). Methods: robotic CNC roughing, precision milling for weight relief, pitch polishing for mid‑spatials, then ion‑beam figuring to dial in λ/10 (or better) form on real parts. Metrology: Fizeau interferometry, surface roughness via white‑light interferometer, and coating durability to ISO 9211‑4; optical surface quality per MIL‑PRF‑13830B. Environmental screens use IEC 60068 series; space programs often ask for GEVS. Service life is project‑dependent, but many customers say 10+ years in labs/observatories is realistic; LEO missions follow their own maintenance/recoat cadence.
| Parameter | Typical value (≈) | Notes |
|---|---|---|
| Substrate | Sitall glass‑ceramic, ultra‑low CTE | Real‑world CTE near 0 ±0.15×10⁻⁶/K |
| Clear aperture | 50–1,200 mm (custom larger) | Batch or one‑off |
| Form accuracy | ≈ λ/10 PV @632.8 nm; RMS 10–15 nm | IBF finish; size dependent |
| Surface roughness | Ra ≤ 0.8 nm | White‑light interferometer |
| Coatings | Al+SiO2; protected Ag; dielectric HR | Reflectivity up to 99.5% (band‑limited) |
| Operating temp | ≈ −40 to +80 °C (typical) | Mission‑dependent |
Case 1: Earth‑observation payload (≈350 mm asphere). After five thermal‑vac cycles, form change was within 25 nm RMS; image chain saw ≈8% MTF stability gain versus an aluminum surrogate. Case 2: Factory line mirror (200 mm line‑scan). Customer reported ~12% throughput improvement and fewer re‑calibrations—small change, big mood lift for ops.
| Vendor | Max aperture | Form (PV) | Lead time | Certs (typ.) | Notes |
|---|---|---|---|---|---|
| Space‑Navi Sitall | ≈1,200 mm | ≈ λ/10 | 6–12 wks | ISO 9001 (req.), ISO 7 cleanroom (≈) | Deep customization, IBF |
| Vendor B | ≈600 mm | ≈ λ/4 | 12–20 wks | ISO 9001 | Good volume pricing |
| Vendor C (EU) | ≈1,000 mm | ≈ λ/8 | 14–24 wks | ISO 9001, 14001 | Premium pricing |
“It seems that the mirror holds figure better after thermal excursions.” Another customer mentioned fewer ghosts with the dielectric HR stack—small but noticeable in HDR scenes. To be honest, real‑world use may vary, but the feedback points to stable alignment and less babysitting. If you’re speccing Camera Mirrors into a schedule‑squeezed program, that’s the whole game.
Each lot ships with interferograms, coating test results (adhesion/abrasion to ISO 9211‑4 or MIL‑PRF‑13830B), and environmental screening data when specified. On request: RoHS statements, material CTE curves, and vibration reports aligned to GEVS or IEC 60068‑2. For procurement, reference drawings using ISO 10110 notation—it saves email ping‑pong.