| Brand Name: | Hoan |
| Model Number: | HALA-CUSTOM-MS |
| MOQ: | 10 Pieces |
| Payment Terms: | L/C,D/A,D/P,T/T,Western Union |
High-reliability and aerospace RF systems operate in environments that make commercial temperature ranges look benign. A SATCOM LNB on a GEO satellite experiences 15 thermal cycles per day between -40°C and +85°C for 15 years — over 80,000 thermal cycles. A high-performance aerospace transceiver system cycles between -55°C at 50,000 feet and +125°C on the tarmac within 30 minutes, while simultaneously vibrating at 20g RMS from 10Hz to 2kHz. An oil well logging tool operates continuously at 185°C with 100g shock loads during tripping operations.
In these environments, an inductor is not a commodity component — it is a single-point failure risk whose reliability directly determines system uptime and safety. The HALA-CUSTOM-SE addresses this reality by combining the inherently robust air-core architecture with high-reliability design practices, severe environment qualification, and full RoHS/REACH compliance with eco-friendly materials throughout.
| Environment | HALA-CUSTOM-SE Capability | Reference Standard |
|---|---|---|
| Operating Temperature | -55°C to +125°C (standard) -55°C to +200°C (PTFE Class C option) |
IEC 60068-2-2 (Dry Heat) IEC 60068-2-1 (Cold) |
| Thermal Shock | -55°C ↔ +125°C, >500 cycles, ΔL <1% | JESD22-A104 (Thermal Cycling) |
| Thermal Vacuum | <1*10⁻⁵ Torr, 1000+ hours, zero outgassing | NASA ASTM E595 (<1% TML, <0.1% CVCM) |
| Random Vibration | 20g RMS, 10Hz–2kHz, 3 axes, 1 hour/axis | IEC 60068-2-64 (Random Vibration) |
| Mechanical Shock | 1500g, 0.5ms half-sine, 5 shocks/axis | IEC 60068-2-27 (Shock) |
| Constant Acceleration | 30,000g, Y1 axis, 1 minute | IEC 60068-2-7 (Steady-State Acceleration) |
| Humidity Resistance | 85°C / 85% RH, 1000 hours, ΔL <2% | IEC 60068-2-78 (Damp Heat Steady State) |
| Salt Atmosphere | 5% NaCl, 35°C, 96 hours | IEC 60068-2-11 (Salt Mist) |
| Solderability | >95% coverage after 8-hour steam age | J-STD-002 / IEC 60068-2-58 |
Why Air Core Outperforms Ferrite in Severe Environments: Ferrite inductors exhibit significant inductance drift under three conditions that define severe environments: temperature (μᵣ changes ~2000ppm/°C for NiZn ferrites), mechanical stress (magnetostrictive inductance modulation under vibration), and radiation (displacement damage reduces μᵣ in ferrite). The air core has none of these failure mechanisms — μ₀ = 1.0 is a universal constant unaffected by temperature, stress, or radiation. For space applications, this means no radiation hardness assurance testing required on the inductor element itself, reducing qualification cost and schedule.
High-Reliability production programs typically involve qualified manufacturing lines with frozen processes — once qualified, the process cannot change without re-qualification. Turn-to-turn consistency at the production stage is therefore not just a quality metric; it is a configuration management requirement.
The HALA-CUSTOM-SE platform delivers production consistency through:
| Control Element | Method | Long-Term Stability |
|---|---|---|
| Mandrel Precision | Carbide mandrel, ±2µm, tungsten carbide (WC) for wear resistance | <±0.5µm diameter drift per 1 million coils |
| Wire Tension Servo | Closed-loop feedback, 0.5–5.0gf, 100Hz control bandwidth | Calibration verified per shift, ±0.1gf drift limit |
| Turn Count Verification | Optical encoder, resolution 0.1° angular position | Zero false-counts across >10 million coils produced |
| Shape Retention | Active shape-lock during extraction, pneumatic precision | Coil deformation <0.3% over 500,000 coils between mandrel replacements |
| In-Line Inspection | 6-axis machine vision, 2µm/pixel, AI defect classification | False-reject rate <0.01%, false-accept rate <10⁻⁶ |
| Per-Coil RF Test | VNA measurement at production rate, automated Go/No-Go binning | Gage R&R <10% of tolerance window |
| Lot Traceability | 2D data matrix on packaging, full digital twin per production lot | Complete material genealogy from wire spool to finished coil |
For programs requiring AS9100 or IATF 16949 production part approval process (PPAP), the HALA-CUSTOM-SE platform supports Level 3 PPAP submissions including: Design Records, Process Flow Diagram, Process FMEA, Control Plan, Measurement System Analysis (MSA), Dimensional Results, Material/Performance Test Results, Initial Process Capability Study (Cpk >1.67), and Part Submission Warrant (PSW).
Environmental compliance in high-reliability/aerospace applications presents a unique challenge: components must meet stringent reliability requirements without relying on the lead-based solders and hazardous materials that historically provided that reliability. The HALA-CUSTOM-SE achieves both objectives through a deliberately simple materials system:
| Material Requirement | HALA-CUSTOM-SE Solution | Compliance Status |
|---|---|---|
| RoHS (2011/65/EU + 2015/863) | Zero Pb, Hg, Cd, Cr⁶⁺, PBBs, PBDEs, DEHP, BBP, DBP, DIBP in any component | Full compliance, per-lot Certificate of Compliance |
| REACH SVHC | Zero Substances of Very High Concern (current Candidate List) in any material | SVHC-free declaration, updated per ECHA Candidate List revision |
| Halogen-Free | Polyurethane and PTFE/polyimide insulation: Br <900ppm, Cl <900ppm, Br+Cl <1500ppm | IEC 61249-2-21 compliant |
| Conflict Minerals | Copper: LME-registered grade A cathode. Tin: conflict-free smelter (CFS) certified. Gold: LBMA Responsible Gold certified. Tungsten (mandrel tooling): CFS certified. | US Dodd-Frank Act Section 1502 / EU Regulation 2017/821 compliant |
| Ozone Depleting Substances | Zero ODS in any manufacturing or cleaning process | Montreal Protocol compliant |
| PFAS (Per- and Polyfluoroalkyl Substances) | PTFE option is a fluoropolymer (not a PFAS surfactant). Manufacturing uses zero PFAS processing aids. | Compliant with emerging PFAS regulations; PFAS-free polyurethane option available |
Eco-Friendly by Design: The three-material bill of materials (copper, tin/gold/silver, polyurethane/PTFE enamel) is inherently simpler than multi-layer ferrite chip inductors that require ceramic powder processing, organic binder burnout, high-temperature sintering (~1200°C), and electroplating with nickel barrier layers. The HALA manufacturing process consumes approximately 80% less energy per unit than equivalent ferrite chip inductor fabrication, and produces zero hazardous waste requiring special disposal.
| Parameter | Value | Qualification |
|---|---|---|
| Temperature Range | -55°C to +125°C (std), +200°C (PTFE) | IEC 60068-2-1 / 60068-2-2 |
| Thermal Shock Endurance | >500 cycles, ΔL <1% | JESD22-A104 |
| Vibration Endurance | 20g RMS, 10Hz–2kHz | IEC 60068-2-64 |
| Mechanical Shock | 1500g, 0.5ms | IEC 60068-2-27 |
| Constant Acceleration | 30,000g, Y1 axis | IEC 60068-2-7 |
| Humidity (85/85) | 1000 hours, ΔL <2% | IEC 60068-2-78 |
| Salt Atmosphere | 96 hours, no corrosion | IEC 60068-2-11 |
| Inductance Range | 2 nH – 500 nH | Per specification |
| Frequency Range | 100 MHz – 20 GHz | Geometry dependent |
| Current Rating | Up to 500 mA DC | Zero saturation, wire gauge dependent |
| Q Factor | ≥100 @ 1 GHz | Air-core, zero hysteresis |
| Solderability (Steam Aged) | >95% coverage | J-STD-002, 8-hour steam age |
| Outgassing (TML) | <1% (standard), <0.1% (space-grade PTFE) | ASTM E595 / NASA |
| Process Cpk | >1.67 | Per-coil RF measurement |
| Compliance | RoHS, REACH, Halogen-Free, CM-Free, ODS-Free | Full per-lot documentation |
| Proto Lead Time | 5–7 business days | MOQ 10 pieces |
Q: Does the HALA-CUSTOM-SE require radiation hardness assurance (RHA) testing?
A: The air core architecture is inherently radiation-immune — there is no semiconductor junction to degrade from TID, no dielectric to charge from deep dielectric charging, and no magnetic domain to disrupt from displacement damage. For programs that require RHA documentation, we provide a Radiation Immunity Analysis Report demonstrating that μ₀ = 1.0 is invariant under all radiation environments up to 100 MeV·cm²/mg LET and 10¹² p/cm² proton fluence. Full RHA testing can be performed on request at program cost.
Q: Can the CUSTOM-SE support Level 3 PPAP for automotive or aerospace programs?
A: Yes. The HALA platform supports Level 3 PPAP including: Design Records, PFMEA, Control Plan, MSA (Gage R&R), Dimensional Results, Material/Performance Test Results, Initial Process Capability Study (Ppk/Cpk >1.67), Appearance Approval Report, and Part Submission Warrant. Contact us during your design phase for PPAP timeline integration.
Contact us with your environmental requirements, qualification standards, and production volume forecast. Mil-spec samples ship in 5–7 business days with MOQ starting at 10 pieces. PPAP and qualification test reports available per program requirements.