AS9100D Quality System
AS9100D supports risk management, configuration control, first article inspection, key-characteristic control, and material traceability for qualified aerospace, defense, and satellite programs.
CNCPioneer manufactures precision satellite housings and spacecraft enclosures in aluminum, titanium, stainless steel, and other specified materials.

A satellite housing is the machined enclosure and reference structure for onboard computers, sensors, payload electronics, propulsion controls, attitude-control hardware, RF systems, and thermal interfaces.
Space hardware also demands low mass, stable geometry, clean processing, controlled materials, and complete documentation.

Coordinate geometry, material, finishing and inspection around the part's intended function.
AS9100D supports risk management, configuration control, first article inspection, key-characteristic control, and material traceability for qualified aerospace, defense, and satellite programs.
MAZAK mill-turn machining supports complete multi-feature housing bodies in fewer setups, helping preserve relationships between pocket geometry, connector cutouts, mounting patterns, flanges, and thermal interfaces.
Rib-and-pocket design, 1.5mm minimum wall guidance, and lightweight alloy selection support mass reduction while maintaining structural stiffness, fastener interfaces, and tool access.
China-based production combines CNC capacity, material supply, and documented inspection to support competitive pricing.
Prototype timing is planned around alloy, machining complexity, surface treatment, inspection, and documentation.
Review mounting faces, pockets and wall thickness before choosing the machining and inspection route.
Explore representative configurations and share your drawing for a product-specific review.

OBC chassis, PCDU housings, AOCS electronics enclosures, transponder bodies, GPS receiver housings, and payload processor chassis.

Star tracker, sun sensor, earth sensor, magnetometer, gyroscope, and IMU housings.

Propulsion electronics housings, pressure transducer bodies, valve housings, sensor enclosures, and electric-propulsion control housings.

Waveguide filter and multiplexer bodies, TWTA and SSPA housings, high-voltage feedthrough interfaces, heat-sink structures, and antenna-control electronics enclosures.

Reaction-wheel housings, control-moment-gyro bodies, magnetorquer housings, rate-gyro bodies, and MEMS IMU enclosures.

Thermal-control electronics housings, loop heat-pipe components, PCM containers, CubeSat electronic stacks from 1U to 12U, sensor heads, and modular SmallSat enclosures.
Match the component to its operating environment, assembly interfaces and documentation requirements.

Satellite Housing Manufacturing for satellite structures, housings and precision interfaces, with material and inspection requirements confirmed for the application.

Transponder chassis, waveguide and multiplexer bodies, TWTA and SSPA enclosures, and antenna-control electronics housings for GEO and LEO communications platforms.

Satellite Housing Manufacturing for satellite structures, housings and precision interfaces, with material and inspection requirements confirmed for the application.

Reconnaissance electronics enclosures, signals-intelligence payload bodies, and strategic-communications chassis with AS9100D quality documentation and configuration control for qualified defense programs.

Atomic-clock housings, navigation-processor chassis, and antenna-electronics enclosures for GPS, Galileo, GLONASS, BeiDou, and other navigation satellite systems.

Satellite Housing Manufacturing for satellite structures, housings and precision interfaces, with material and inspection requirements confirmed for the application.
Explore machining capabilities, material options and quality support for satellite components.
Explore satellite machiningMaterials
Confirm the exact grade, delivery condition and finish compatibility with your drawing.
Aluminum options for lightweight machined components. Confirm the alloy, temper, finishing allowance and critical assembly dimensions.
Aluminum options for lightweight machined components. Confirm the alloy, temper, finishing allowance and critical assembly dimensions.
High-cycle mechanism satellite housings, fatigue-critical structural elements, vibration-isolated instrument enclosures · TML <0.1% · CTE 23.2 ppm/°C · Superior fatigue resistance for deployable mechanism and vibration-critical satellite housing applications.
CFRP interface satellite housings, propulsion system housings, high-load structural enclosures · TML <0.05% · Density 4.43 g/cm³ · CTE 8.6 ppm/°C · 40% lighter than steel · Excellent fatigue resistance and propellant compatibility for satellite propulsion environments.
Non-magnetic sensor satellite housings, magnetometer enclosures, attitude determination instrument housings · TML <0.1% · CTE 16.0 ppm/°C · Austenitic microstructure: magnetic permeability below 1.02μr · Mandated for magnetometer and magnetic cleanliness satellite applications.
High-load compact satellite housings, structural electronics enclosures, valve seat housings · TML <0.1% · CTE 10.8 ppm/°C · Tensile 1,310 MPa · Maximum yield strength in compact cross-sections for satellite mechanism and structural applications.
Propulsion valve satellite housings, high-pressure service enclosures, deployment mechanism springs · TML <0.1% · CTE 12.8–13.0 ppm/°C · Creep and stress rupture resistant for high-temperature satellite propulsion system housings and hot section components.
Optical instrument satellite housings, telescope structure enclosures, precision reference housings · CTE 1.3 ppm/°C · TML <0.1% · Dimensional stability across orbital thermal cycling that earth observation and science satellite optical system performance budgets require.
Finish selection
Select the finish around the specified material, functional surfaces and service conditions. Confirm process details and acceptance requirements with your drawing.
Review hard anodizing against the material, functional surfaces and intended service conditions.
Standard corrosion protection anodize for aluminum satellite housing internal surfaces and non-wear-surface external features.
Alodine chromate conversion coating for aluminum satellite housing hardware requiring electrical conductivity for satellite structure grounding, RF shielding continuity, and ESD protection.
Nitric or citric acid passivation for stainless steel and titanium satellite housing components — propulsion valve housings, sensor body elements, and instrument housing hardware.
Hard gold plating for satellite housing electrical contact surfaces — RF connector contacts, electrical connector pins, slip ring interfaces, and grounding contact hardware.
Review silver plating for rf satellite housings against the material, functional surfaces and intended service conditions.
Machining resources for drawing review, prototypes and repeat-production programs.
Inspection & documentation
Review material identity, machining datums, functional dimensions and production records for your component.
Final tolerances, inspection coverage and acceptance criteria are confirmed against your drawing, material and geometry.
Confirm the certificates, inspection reports and production records needed for your order when sharing your drawing.
The product range includes Electronic Unit Satellite Housings, Sensor & Instrument Satellite Housings, Propulsion System Satellite Housings. Custom geometry is reviewed against the approved drawing.
Material options include 6061-T6, 7075-T6, 2024-T351. The exact grade and condition should be confirmed for your application.
Define mounting faces, pockets and wall thickness, together with datums, tolerances and required surface condition.
Finishing options include hard anodizing, type ii anodizing, chemical film. Applicability is reviewed against the specified material and geometry.
Pricing and delivery are confirmed after reviewing the drawing, material availability, quantity, machining route, finishing and inspection scope.
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Share your drawing or 3D model, material, critical dimensions, finish and order quantity. We’ll review the machining route, inspection scope and delivery requirements.