Radiation effects & COTS screening
Also known as TID, SEU, SEL, SAA
Total ionizing dose (TID), single-event upsets (SEU) and destructive latch-up (SEL) in the South Atlantic Anomaly for 500–600 km COTS avionics.
- Document
- SQ-EN-005
- Updated
- Reading time
- 1 min
In this tab
Total ionizing dose vs single-event effects in LEO
At Sun-synchronous orbits, a PocketQube has relatively thin shielding—often of aluminium or of FR-4—yet its short orbital lifetime () keeps cumulative Total Ionizing Dose () around [1]. Most modern commercial off-the-shelf () CMOS microcontrollers, transceivers and LDOs survive without parametric failure[2].
The primary radiation hazard in is instead Single-Event Effects () triggered by high-energy protons () trapped in the South Atlantic Anomaly (SAA) and galactic cosmic rays near the poles[3]:
- Single-Event Upset (): Non-destructive bit flip in SRAM, processor registers or flash configuration cells.
- Single-Event Latch-up (): Parasitic thyristor triggering in bulk CMOS that creates a low-impedance short between supply and ground, destroying the IC thermally unless power is cut within milliseconds.
Circuit and architectural mitigations
- Per-rail over-current foldback and power cycling: Every subsystem rail on the EPS is routed through a fast current-limiting switch () that quenches currents and re-powers the branch after a cooldown delay[2].
- FRAM and MRAM for critical state: Ferroelectric RAM (e.g., TI MSP430FR series or external SPI FRAM) stores boot counters, orbital parameters and configuration tables in polarization states immune to proton bit flips, paired with Triple Modular Redundancy (TMR) and CRC-32 scrubbing[3].
References
- [1]European Cooperation for Space Standardization. (2020). ECSS-E-ST-10-04C Rev.1: Space engineering — Space environment. ESA Requirements and Standards Section.ecss.nl(accessed 20 October 2026)
- [2]nadir lab. (2026). PocketQube-class picosatellites: architecture, flight heritage, and a multi-method post-flight analysis of Grizu-263A [Preprint]. nadir lab. Research Monographs (SQ-R-001).Read on nadir lab.
- [3]NASA Small Spacecraft Systems Virtual Institute. (2026). Small Spacecraft Avionics. State-of-the-Art of Small Spacecraft Technology (2026 edition), Chapter 8. NASA Ames Research Center.nasa.gov(accessed 20 October 2026)
Cite this SatWiki entry
@misc{nadirlab2026radiation,
author = {{nadir lab.}},
title = {{Radiation effects \& COTS screening}},
year = {2026},
month = oct,
howpublished = {nadir lab. SatWiki SQ-EN-005 (Rev. 1)},
url = {https://nadirlab.space/wiki/radiation-effects/}
}nadir lab. (2026). Radiation effects & COTS screening. nadir lab. SatWiki (SQ-EN-005, Rev. 1). https://nadirlab.space/wiki/radiation-effects/
TY - ENCYC AU - nadir lab. TI - Radiation effects & COTS screening T2 - nadir lab. SatWiki PY - 2026 ET - Rev. 1 C1 - SQ-EN-005 UR - https://nadirlab.space/wiki/radiation-effects/ ER -