Precision-Crafted Space Components

According to our CNC machining knowledge base, aerospace CNC machining achieves tolerances as tight as 0.002mm. For space components, we routinely hold positional tolerances to ±0.002mm, concentricity to ±0.003mm, and surface flatness to ±0.002mm. Every part is inspected on a Hexagon coordinate measuring machine (CMM) with accuracy verification to 4 microns.

Yes. Every lot is locked to the original mill-test report (MTR) at receipt. Traceability is maintained through machining, heat treatment, surface finishing, and final packaging. A certificate of conformance (CoC) with material pedigree ships with every order, meeting AS9100D and customer-specific requirements. ITAR-controlled programs receive additional documentation controls.

Ti-6Al-4V ELI is the preferred alloy for primary satellite structures, offering 50% weight savings over steel with 30% greater strength. For secondary structures and thermal management, 7075-T6 aluminum delivers 83 ksi UTS with excellent machinability. For propulsion systems, Inconel 718 withstands temperatures to 650°C. We will recommend the optimal alloy based on your mission mass budget and thermal environment.

Yes. Our 5-axis simultaneous machining centers produce regenerative cooling channels with wall thicknesses as low as 0.8mm in Inconel 718. We use through-spindle coolant and ceramic tooling at optimized speeds to maintain surface integrity. Every nozzle throat is CMM-verified for concentricity and profile accuracy before delivery.

Yes. All polymer-adjacent processes and surface treatments are screened for outgassing per ASTM E595. Total mass loss (TML) is verified below 1.0% and collected volatile condensable materials (CVCM) below 0.10% for instrument housings and optical benches. We can provide outgassing test reports with every shipment.

First articles: 2–3 weeks. Production lots: 4–6 weeks depending on material availability and NDT requirements. For critical path items, we offer expedited programs with dedicated machine time. We maintain raw material stock for common aerospace alloys including Ti-6Al-4V, 7075-T6, and Inconel 718 to reduce procurement delays.

All structural components are designed with stress-relief radii and optimized wall thicknesses per NASA-STD-7003. We perform random vibration qualification testing up to 14 Grms across 20–2,000 Hz on electrodynamic shakers. Finite element analysis (FEA) is available to predict modal response before hardware is committed.

Yes. We are ITAR registered and maintain compliant facility access controls, document security, and personnel screening. ITAR programs receive segregated manufacturing cells, controlled access to drawings, and encrypted data transfer. Our quality system addresses ITAR requirements as part of AS9100D document control.