A vacuum outgassing PCB built on a ceramic substrate produces negligible volatile contamination because the fired inorganic body—Al₂O₃, AlN, or Si₃N₄—contains no polymer binder to release trapped gases. A 96% alumina substrate tested per ASTM E595 typically shows total mass loss (TML) below 0.01% and collected volatile condensable material (CVCM) below 0.001%, far under NASA’s screening limits of 1.0% TML and 0.1% CVCM. That makes ceramic the default substrate choice when contamination-sensitive optics, sensors, or spacecraft surfaces share the same vacuum volume as the circuit board.
Any material placed inside a vacuum chamber or launched into orbit will release trapped gases and volatile organic compounds. Those volatiles condense on cooler surfaces—mirror coatings, detector windows, solar cells—degrading optical transmission and electrical performance. NASA’s ASTM E595 test (24 h at 125 °C, ≤5 × 10⁻⁵ torr) is the standard screening method. Components that exceed 1.0% TML or 0.1% CVCM are flagged for replacement or additional bake-out.
FR-4 (glass-epoxy) fails this screen easily: published TML values for standard FR-4 range from 0.5% to 1.8%, depending on resin system and moisture content, per NASA’s outgassing database. Polyimide flex (e.g., Kapton-based) performs better—TML around 0.9–1.2%—but still sits close to the limit and requires extended bake-out. A vacuum outgassing PCB built on ceramic sidesteps the problem entirely because there is no organic matrix to degas.

| Material | TML (%) | CVCM (%) | Test Standard | Source |
|---|---|---|---|---|
| Al₂O₃ 96% | < 0.01 | < 0.001 | ASTM E595 | CoorsTek ADS-96R datasheet |
| Al₂O₃ 99.6% | < 0.01 | < 0.001 | ASTM E595 | Kyocera A-493 datasheet |
| AlN | < 0.01 | < 0.001 | ASTM E595 | Maruwa AN-230 datasheet |
| Si₃N₄ | < 0.01 | < 0.001 | ASTM E595 | Kyocera SN-220 datasheet |
| FR-4 (typical) | 0.5–1.8 | 0.02–0.15 | ASTM E595 | NASA GSFC outgassing database |
| Polyimide flex | 0.9–1.2 | 0.01–0.05 | ASTM E595 | NASA GSFC outgassing database |
Typical values for commercially available material, for comparison only. Confirm against the datasheet for your specific grade.
The ceramic substrate itself is not the whole story. Every material on the finished board contributes to total outgassing: solder paste flux residue, conformal coating, adhesives, and even surface finish chemistry. A vacuum outgassing PCB with a pristine ceramic substrate can still fail ASTM E595 if assembled with standard no-clean flux and not properly cleaned afterward.
Because the ceramic body contributes essentially zero volatiles, the outgassing budget of a finished ceramic assembly is dominated by these secondary sources:
Selecting a ceramic substrate is the first step. The rest of the design must follow vacuum-compatible practices. Here is a practical checklist:
Following ceramic PCB design guidelines from the start avoids late-stage redesigns that can introduce non-compliant materials.
Enter your substrate material, operating temperature, and environment below to see how thermal derating affects your vacuum outgassing PCB design margins.
Consider a 25 × 25 mm Al₂O₃ 96% board carrying a MEMS sensor, assembled with SAC305 solder and ENIG finish, cleaned per IPC J-STD-001 Class 3, and baked out at 125 °C for 48 h.
Board mass: ~3.8 g (alumina density 3.7–3.9 g/cm³, 0.635 mm thick). At TML < 0.01%, the substrate contributes < 0.38 µg of mass loss. The dominant outgassing source is the die-attach adhesive—say 5 mg of silver epoxy at TML 0.53%, contributing ~26.5 µg. Total assembly TML is driven almost entirely by the adhesive, not the board. This illustrates why material selection for attach and encapsulation matters more than the substrate itself once you have chosen ceramic for your vacuum outgassing PCB.

| Parameter | Ceramic (Al₂O₃ 96%) | Polyimide Flex | FR-4 |
|---|---|---|---|
| TML (ASTM E595) | < 0.01% | 0.9–1.2% | 0.5–1.8% |
| CVCM (ASTM E595) | < 0.001% | 0.01–0.05% | 0.02–0.15% |
| Max continuous temp | 300–800 °C (material-dependent) | 200–260 °C | 130–140 °C |
| Thermal conductivity | 24–28 W/mK | 0.2–0.4 W/mK | 0.3–0.4 W/mK |
| CTE (ppm/°C) | 6.5–7.2 | 12–20 | 14–17 |
| Relative cost | 5–15× FR-4 | 2–5× FR-4 | 1× |
| Bake-out required? | Recommended (short) | Required (extended) | Often fails even after bake-out |
Typical values for commercially available material, for comparison only. Confirm against the datasheet for your specific grade.
Ceramic is not always the right answer, even in vacuum. Consider alternatives when:
Space hardware faces repeated thermal vacuum (TVAC) cycles, often −55 °C to +125 °C. Ceramic substrates handle this range without degradation—alumina’s flexural strength (300–380 MPa per ASTM C1161) does not change meaningfully across this band. The weak point is the solder joint, especially where CTE mismatch exists between the ceramic (6.5–7.2 ppm/°C) and a component package (e.g., plastic QFP at 15–20 ppm/°C). Minimize large-footprint plastic packages, prefer leadless ceramic chip carriers or bare die, and qualify joints with thermal cycling per IPC-9701. For more on managing ceramic thermal management under TVAC conditions, review your thermal stack early in the design phase.
Yes, but the bake-out is short—typically 24 h at 100–125 °C. The ceramic itself holds negligible volatiles; the bake-out targets adsorbed water and trace residues from assembly materials. FR-4 and polyimide boards require 48–72 h or longer under the same conditions.
You can use standard SAC305 alloy, but you must fully clean the flux residue after reflow. No-clean flux is not acceptable for vacuum service because the residue outgasses organic compounds. Specify water-soluble flux with post-reflow aqueous cleaning and ionic contamination verification.
ENIG (electroless nickel / immersion gold) is the most common choice. It is inorganic, solderable, wire-bondable, and adds no measurable outgassing. ENEPIG adds a palladium barrier and is preferred when both gold wire bonding and soldering are needed on the same board. Avoid OSP, which is an organic finish.
Yes. LTCC (low-temperature co-fired ceramic) is used extensively in space-qualified RF modules and hermetic packages. The co-fired glass-ceramic body is fully sintered and contains no organics after firing. Outgassing is comparable to alumina substrates. Embedded conductors are typically silver or gold, both inorganic.
You test the complete assembly, not just the substrate. Submit a representative coupon—same materials, same process, same cleaning—to a lab accredited for ASTM E595 (e.g., NASA GSFC, Jet Propulsion Laboratory, or commercial labs like NTS or EAG Laboratories). Turnaround is typically 2–4 weeks. Many programs accept manufacturer-published data for individual materials combined into a worst-case outgassing budget, but flight qualification usually requires assembly-level testing.
If you are specifying a vacuum outgassing PCB on ceramic for space or high-vacuum service, start with a DFM review to catch material and process choices that could compromise outgassing performance. Review ceramic PCB application examples for similar projects, then upload your files for a quote and flag the vacuum requirement so the engineering team can recommend the right substrate, metallization, and cleaning process for your contamination budget.