Vacuum outgassing screening (TML and CVCM)#
Under -Q-ST-70-02C[1] and ASTM E595, polymeric materials heated at for at must satisfy[2]:
where Total Mass Loss (TML) measures total volatile release and Collected Volatile Condensable Material (CVCM) measures the fraction that condenses on a collector plate held at [3]. On a cube, any silicone adhesive or plasticized PVC wire jacket outgasses directly onto adjacent solar coverglasses and camera lenses within centimetres.
| Material | TML | CVCM | WVR | RML | Screening | Erosion yield (10⁻²⁴ cm³/atom) | Recession, tumbling face (µm/yr) |
|---|---|---|---|---|---|---|---|
| FR-4 laminate | 0.22 | 0.00 | 0.09 | 0.13 | Passes ECSS and ASTM | — | — |
| G-10 laminate | 0.52 | 0.00 | 0.16 | 0.36 | Passes ECSS and ASTM | — | — |
| Polyimide–glass laminate | 0.71 | 0.00 | 0.40 | 0.31 | Passes ECSS and ASTM | — | — |
| PEEK, moulded | 0.14 | 0.00 | 0.05 | 0.09 | Passes ECSS and ASTM | 2.99 | 16 |
| PEI (Ultem), moulded | 0.40 | 0.00 | 0.32 | 0.08 | Passes ECSS and ASTM | > 3.31 | 18 |
| ULTEM 1010, FDM (XY) | 0.55 | 0.02 | 0.39 | 0.16 | Passes ECSS and ASTM | — | — |
| Polypropylene filament | 0.24 | 0.05 | 0.03 | 0.21 | Passes ECSS and ASTM | — | — |
| Polyimide film (Kapton)Erosion-yield reference | 0.97 | 0.00 | 0.80 | 0.17 | Passes ECSS and ASTM | 3 | 16 |
| PET film (Mylar) | 0.24 | 0.01 | 0.18 | 0.06 | Passes ECSS and ASTM | 3.01 | 16 |
| PTFE | 0.01 | 0.00 | 0.02 | −0.01 | Passes ECSS and ASTM | 0.142 | 0.8 |
| ABS | — | — | — | — | Grade-dependent | 1.09 | 5.8 |
| Polyamide 6 | — | — | — | — | Grade-dependent | 3.51 | 19 |
TML, CVCM, WVR and RML = TML − WVR in per cent; limits 1.0% mass loss and 0.10% CVCM (ECSS-Q-ST-70-02C on RML, ASTM E595 on TML). Recession = erosion yield × fluence, using the ISS ram fluence of MISSE-2 (2.1 × 10²¹ atoms/cm² a year) divided by four for a tumbling face; at 500–550 km the fluence is lower.
4.5 eV atomic oxygen and surface recession#
Photodissociation of by solar ultraviolet radiation makes monatomic oxygen () the dominant neutral species between and [4]. At an orbital speed , impacting oxygen atoms carry translational energy —sufficient to break and bonds. For a material with erosion yield () exposed to annual fluence (), the surface recession depth is[5]:
| Polymer / coating | Erosion yield E_y (cm³/atom) | Recession depth (µm) | Mass loss (mg/cm²) | Engineering notes |
|---|---|---|---|---|
| Kapton HN (polyimide) | 3.00 × 10⁻²⁴ | 70.5 | 10.02 | Standard reference material (ASTM E2089); rapid unprotected erosion below 450 km. |
| FR-4 / Epoxy matrix | 2.10 × 10⁻²⁴ | 49.4 | 9.14 | Glass fibres remain intact after resin matrix erodes, creating a diffuse matte surface. |
| FEP / PTFE (Teflon) | 3.50 × 10⁻²⁵ | 8.2 | 1.77 | Low atomic-oxygen yield alone, but synergistic VUV + AO accelerates degradation. |
| PEEK structural polymer | 2.30 × 10⁻²⁴ | 54.1 | 7.14 | Used in antenna deployment spools and insulating standoffs. |
| SiOx-coated Kapton (130 nm) | 2.00 × 10⁻²⁶ | 0.5 | 0.07 | Passivating silica barrier cuts effective erosion by > 98% outside pinhole defects. |
Interactive polymer erosion calculator#
Use the interactive model below to evaluate annual fluence and recession depth across altitude, mission duration and solar activity:
| Polymer / coating | Erosion yield E_y (cm³/atom) | Recession depth (µm) | Mass loss (mg/cm²) | Engineering notes |
|---|---|---|---|---|
| Kapton HN (polyimide) | 3.00 × 10⁻²⁴ | 70.5 | 10.02 | Standard reference material (ASTM E2089); rapid unprotected erosion below 450 km. |
| FR-4 / Epoxy matrix | 2.10 × 10⁻²⁴ | 49.4 | 9.14 | Glass fibres remain intact after resin matrix erodes, creating a diffuse matte surface. |
| FEP / PTFE (Teflon) | 3.50 × 10⁻²⁵ | 8.2 | 1.77 | Low atomic-oxygen yield alone, but synergistic VUV + AO accelerates degradation. |
| PEEK structural polymer | 2.30 × 10⁻²⁴ | 54.1 | 7.14 | Used in antenna deployment spools and insulating standoffs. |
| SiOx-coated Kapton (130 nm) | 2.00 × 10⁻²⁶ | 0.5 | 0.07 | Passivating silica barrier cuts effective erosion by > 98% outside pinhole defects. |