DOC // NL-TN-2026-014VECTOR -Z1P / 1U · MATERIALS · ORBITAL
STATUS: PUBLISHED // REV 0.1

Atomic oxygen and polymers in low Earth orbit

Vacuum outgassing screening, 4.5 eV ram atomic-oxygen fluence and surface recession of Kapton, PEEK, PTFE and FR-4

Author
nadir lab.
Published
Reading time
2 min
Level
Academic
Tags
  • Atomic oxygen
  • Outgassing
  • Polymers
  • Kapton
  • Materials
  • PocketQube

Abstract

Polymers on the exterior of a PocketQube—solar-panel substrates, Kapton insulation, PEEK spools, UHMWPE burn lines and exposed FR-4 edges—face both high-vacuum volatile condensation and 4.5 eV ram atomic oxygen (AO). We review ECSS-Q-ST-70-02C / ASTM E595 screening limits and compute annual AO fluence and recession depth from 350 to 600 km.

Contents

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.

Outgassing screening and atomic-oxygen recession of polymers
MaterialTMLCVCMWVRRMLScreeningErosion yield (10⁻²⁴ cm³/atom)Recession, tumbling face (µm/yr)
FR-4 laminate0.220.000.090.13Passes ECSS and ASTM——
G-10 laminate0.520.000.160.36Passes ECSS and ASTM——
Polyimide–glass laminate0.710.000.400.31Passes ECSS and ASTM——
PEEK, moulded0.140.000.050.09Passes ECSS and ASTM2.9916
PEI (Ultem), moulded0.400.000.320.08Passes ECSS and ASTM> 3.3118
ULTEM 1010, FDM (XY)0.550.020.390.16Passes ECSS and ASTM——
Polypropylene filament0.240.050.030.21Passes ECSS and ASTM——
Polyimide film (Kapton)Erosion-yield reference0.970.000.800.17Passes ECSS and ASTM316
PET film (Mylar)0.240.010.180.06Passes ECSS and ASTM3.0116
PTFE0.010.000.02−0.01Passes ECSS and ASTM0.1420.8
ABS————Grade-dependent1.095.8
Polyamide 6————Grade-dependent3.5119

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]:

Atomic oxygen fluence and polymer erosion depth at 400 km over 2 year(s) (F10.7 = 140 sfu, ram factor 0.32)
Polymer / coatingErosion yield E_y (cm³/atom)Recession depth (µm)Mass loss (mg/cm²)Engineering notes
Kapton HN (polyimide)3.00 × 10⁻²⁴70.510.02Standard reference material (ASTM E2089); rapid unprotected erosion below 450 km.
FR-4 / Epoxy matrix2.10 × 10⁻²⁴49.49.14Glass fibres remain intact after resin matrix erodes, creating a diffuse matte surface.
FEP / PTFE (Teflon)3.50 × 10⁻²⁵8.21.77Low atomic-oxygen yield alone, but synergistic VUV + AO accelerates degradation.
PEEK structural polymer2.30 × 10⁻²⁴54.17.14Used in antenna deployment spools and insulating standoffs.
SiOx-coated Kapton (130 nm)2.00 × 10⁻²⁶0.50.07Passivating 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:

Atomic oxygen fluence and polymer erosion depth at 400 km over 2 year(s) (F10.7 = 140 sfu, ram factor 0.32)
Polymer / coatingErosion yield E_y (cm³/atom)Recession depth (µm)Mass loss (mg/cm²)Engineering notes
Kapton HN (polyimide)3.00 × 10⁻²⁴70.510.02Standard reference material (ASTM E2089); rapid unprotected erosion below 450 km.
FR-4 / Epoxy matrix2.10 × 10⁻²⁴49.49.14Glass fibres remain intact after resin matrix erodes, creating a diffuse matte surface.
FEP / PTFE (Teflon)3.50 × 10⁻²⁵8.21.77Low atomic-oxygen yield alone, but synergistic VUV + AO accelerates degradation.
PEEK structural polymer2.30 × 10⁻²⁴54.17.14Used in antenna deployment spools and insulating standoffs.
SiOx-coated Kapton (130 nm)2.00 × 10⁻²⁶0.50.07Passivating silica barrier cuts effective erosion by > 98% outside pinhole defects.

References

  1. [1]nadir lab. (2026). Materials engineering for PocketQube picosatellites: A scaling-based review and design guide [Preprint]. nadir lab.Read on nadir lab.
  2. [2]European Cooperation for Space Standardization. (2008). ECSS-Q-ST-70-02C: Space product assurance — Thermal vacuum outgassing test for the screening of space materials. ESA-ESTEC.
  3. [3]ASTM International. (2021). ASTM E595-15(2021): Standard test method for total mass loss and collected volatile condensable materials from outgassing in a vacuum environment. ASTM International.
  4. [4]Banks, B. A., Backus, J. A., & de Groh, K. K. (2008). Atomic oxygen erosion yield predictive tool for spacecraft polymers in low Earth orbit (NASA/TM-2008-215490). NASA Glenn Research Center.
  5. [5]de Groh, K. K., Banks, B. A., McCarthy, C. E., Rucker, R. N., Roberts, L. M., & Berger, L. A. (2008). MISSE 2 PEACE polymers atomic oxygen erosion experiment on the International Space Station. High Performance Polymers, 20, 388–409.

Cite this article

@misc{nadirlab2026atomic,
  author       = {{nadir lab.}},
  title        = {{Atomic oxygen and polymers in low Earth orbit}},
  year         = {2026},
  month        = oct,
  howpublished = {nadir lab. nadir lab. technical note SQ-TN-2026-014},
  url          = {https://nadirlab.space/en/articles/atomic-oxygen-and-polymers/},
  language     = {english},
  note         = {Licence: CC BY 4.0}
}
DOI
Not assigned
Identifier
SQ-TN-2026-014
Licence
CC BY 4.0