Title: Space Radiation Effects in Electronic Components.
1Space Radiation Effectsin Electronic Components.
- Len Adams
- Professor Associate, Brunel Univ.
- Consultant to Spur Electron.
- For PA and Safety Office.
- May 2003
2Space Radiation Effects in Electronic
ComponentsStructure of Presentation
- Space radiation environment
- Radiation effects in electronic components.
- Radiation testing
- Use of commercial components
- Guide to comrad-uk resource
- Open discussion
3Space Radiation EnvironmentOverview
- Complex and Dynamic
- Trapped Radiation Belts of energetic
electrons and protons - Cosmic Rays (Energetic Ions)
- Solar Event protons
4Space Radiation EnvironmentTrapped Radiation
- Electrons and Protons are trapped in the Earths
magnetic field, forming the Van Allen belts. - Electrons up to 7 MeV
- Protons up to a few hundred MeV.
5Electron Belts
6Proton Belts
7Space Radiation EnvironmentTransiting Radiation
- Very high energy Galactic Cosmic Rays originating
from outside the solar system - Solar Events. (X-rays, protons and heavy ions)
8Space Radiation EnvironmentGalactic Cosmic Rays
- 85 Protons, 14 Alpha particles, 1 Heavy
Nuclei. - Energies up to GeV
- Expressed in terms of Linear Energy Transfer
(LET) for radiation effects purposes
9Space Radiation EnvironmentSolar Flares
- Occur mostly near first and last year of solar
maximum - Solar Events, composed mainly of protons with
minor constituent of alpha particles, heavy ions
and electrons
10Space Radiation EnvironmentSouth Atlantic Anomaly
- Distortion of the earths magnetic field allows
the proton belts to extend to very low altitudes
in the region of South America - Low Earth Orbiting satellites will be exposed to
high energy protons in this region
11Space Station. 1 year dose-depth curve.
12Space Station . Non-Ionizing Energy Loss
spectrum.
13Space Station. Orbit averaged LET spectra
14Space Station. Proton flux as a function of
orbital time.
15Radiation Effects in Components(1) IONIZATION
- Mechanism Charge generation, trapping and
build-up in insulating layers. - Due to Electrons, Protons.
- Main Effects Parameter drift. Increased leakage
currents. Loss of noise immunity. Eventual
functional failure
16Radiation Effects in Components(2) DISPLACEMENT
DAMAGE
- Mechanism Disruption of crystal lattice
- Due to Protons
- Main Effects Reduced gain, increased ON
resistance, reduced LED output, reduced charge
transfer efficiency in CCDs.
17Radiation Effects in Components(3) SINGLE EVENT
- Mechanism Dense path of localised ionization
from a single particle hit - Due to Cosmic rays, high energy protons.
- Main Effects Transient current pulses, variety
of transient and permanent Single Event Effects
18Single Event Current Pulse
19SEU Mechanism in CMOS bistable
20Radiation Effects in Components(4) Single Event
Effects in detail
- Latch-up. Permanent, potentially destructive
- Bit flips (Single Event Upset) in bistables
- High Anomalous Current (HAC), snap-back
- Heavy Ion Induced Burn-out in power MOS
- Single Event Gate Rupture (SEGR)
- Single Event Transient, noise pulses, false
outputs - Soft Latch (device or system lock up)
21Typical Single Event Transient Requirements.
- Output voltage swing of rail voltage to ground
and ground to rail voltage. - Duration
- 15 microseconds for Op-Amps.
- 10 microseconds for comparators, voltage
regulators and voltage references. - 100 nanoseconds for opto-couplers.
22Radiation TestingSpecifications and Standards
- Total Ionizing Dose
- SCC-22900 (ESA-SCC)
- Mil Std 883E Method 1019.6 (DESC)
- ASTM F1892 (includes ELDRS)
- Single Event
- SCC-29500 (ESA-SCC)
- EIA/JEDEC Standard EIA/JESD57
- ASTM F1192
23Radiation TestingImportant Considerations
- Choice of radiation source.
- Specifications and Standards
- Worst case or application bias
- Test software
- Number of samples
- Traceability
- Databasing
24Radiation TestingChoice of Source
- Total Ionizing Dose Co-60 gamma or
- 1-3 MeV electrons (Linac or VdG)
- Displacement Damage Protons (10-20 MeV),
Neutrons (1 MeV), Electrons (3-5 MeV) - Single Event Heavy Ion Accelerator (ESA-Louvain
HIF), Proton Accelerator (ESA-PSI PIF) - Cf-252 CASE laboratory system.
-
25Typical Radiation Verification (RVT) requirements.
TECHNOLOGY REQUIREMENT DOSE RATE
Bipolar Transistor Data gt 10 yrs High or Low
MOS Transistor All diffusion lots High or Low
Linear ICs All diffusion lots Low
MOS Digital ICs Data gt 1 yr High or Low
Bipolar Digital ICs Data gt 10 yrs Low
ASICs, FPGA. Data gt 2 yrs Low
MOS RAM, ROM Data gt 2 yrs High or Low
Bipolar RAM, ROM Data gt 6 yrs Low
Optoelectronics All diffusion lots High or Low
26Technologies generally considered to be radiation
tolerant ( 300 krad)
- Diodes (other than zener).
- TTL logic (e.g. 54xx series).
- ECL (Emitter Coupled Logic).
- GaAs (Gallium Arsenide) technologies.
- Microwave devices.
- Crystals.
- Most passives.
27Radiation TestingSample Size/Traceability
- Sample Size
- Total Ionizing Dose. Minimum 5 samples. 4 test,
1 reference. - Single Event. 3 samples recommended.
- Traceability
- Use single Lot-Date-Code for test and flight
hardware. -
28Dose-rates for testing.
- - High Dose Rate
- SCC 22900 Window 1. 1-10 rads/sec.
- MIL883E 1019.6. 50-300 rads/sec.
- Low Dose Rate
- SCC 22900 Window 2. 0.01-0.1 rads/sec.
- MIL883E 1019.6. 0.01 rads/sec.
- Elevated Temp. 0.5-5 rads/sec.
29Radiation TestingTest Software (Single Event)
- Test pattern dependence. All 1, All 0, Alternate
1-0, Chequerboard, MOVI. - Different sensitivities for different registers.
- Dead Time. (detect flip/record/rewrite)
- How to test Processors (Golden Chip ?)
- Possibility to run application software ?
- Beware of software/hardware interaction.
30Radiation TestingAnd finally
- TEST IT LIKE YOU FLY IT
- FLY IT LIKE YOU TEST IT
- (Ken LaBel. GSFC)
31Use of Commercial Components
- The use of commercial technology does NOT
necessarily result in cost-saving. - Cost of Ownership is the important consideration.
- First choice should always be QML or Space
Quality components if available.
32Why Use Commercial Technology ?
- Complexity of functions
- Performance
- Availability (limited number of QML/Space
suppliers).
33What are the drawbacks of commercial technology?
- Little or no traceability
- Rapid and unannounced design and process changes.
- Rapid obsolescence
- Packaging Issues (Plastic).
- - Effect of burn-in on radiation response
- - Deep dielectric charging in space (?)
34COTS Hardness Assurance
- Define the hazard
- Evaluate the hazard
- Define requirements
- Evaluate device usage
- Discuss with designers
- Iterate process as necessary
35Risk Assessment Mitigation
- Components list review by a radiation expert
- Good Radiation Design Margin (2-5)
- Fully characterise key components
- Limit the use of new technologies
- Eliminate or shield marginal technologies
- Maintain awareness of developments in radiation
effects - Do not cut back on testing
- Look for system solutions
36Countermeasures/MitigationTotal Ionizing Dose.
- Additional shielding. Only effective in electron
dominated environments. - Cold redundancy (sparing). Not effective for
all technologies. - Generous derating.
- Robust electronic design. High drive currents,
low fan-out or loading. Large gain margins, high
noise immunity etc.
37Countermeasures/Mitigation. Single Event Effects
- Note that additional shielding is NOT effective.
- Ensure systems are not sensitive to transient
effects. - Use fault tolerant design techniques.
- Use Error Detection and Correction for critical
circuits. - Ensure systems can re-boot autonomously.
38COMRAD-UKAn integrated Web resource of
components radiation effects data.
39Why Integrated Web Resource ?
- COMRAD provides more than a database.
- it includes
- Components radiation effects database.
- A tutorial handbook.
- Links to radiation effects sites.
- Links to manufacturers sites.
- Links to publications in .pdf format.
- Experts Forum for technical discussions.
40Available from COMRAD-UK Home Page
Terms Links Glossary
Index Search Total Dose
Heavy Ion Neutron Proton
Sponsors Manufacturers Seminars
Handbook Publications News Experts Forum
41(No Transcript)
42 Origins of COMRAD-UK Database
- ESA RADFX (on discs)
- Database Round Table (RADECS 1993)
- Discussions with Space Agencies, Scientific
Institutes and Industry - Discussions with CERN LHC Project and Detector
groups.
43Aims of COMRAD-UK Database
- To be informative not regulatory.
- To contain recent data and be continuously
updated. - To provide data summary and detailed tabulated
data (if available). - To provide contact details for the test
authority. - To be expandable for High-Energy Physics and
Avionics
44COMRAD-UK Database status.
- 700 Total Dose records
- 280 Single Event Records
- Being updated on a monthly basis
- Primary data resources
- IEEE NSREC Data Workshop and Proceedings
- RADECS Data Workshop and Proceedings
- ESA Contract Reports.
- IEEE Publications.
- CERN reports and publications
45 Origins of COMRAD-UK Handbook
- ESA Radiation Design Handbook. PSS-609
- Handbook of Radiation Effects. OUP 1993.
- The use of commercial components in aerospace
technology. BNSC Contract Report 1999. - Participation in CERN RD-49 collaboration.
Hardened microelectronics and commercial
components. - Various international seminars and workshops over
past 5 years.
46 Aims of COMRAD-UK Handbook
- A brief (100 page) tutorial guide to the space
application of components. - To assist in the assessment of components in the
COMRAD database for any particular mission. - Provides guidance on Hardness Assurance
practices. - Discusses the application of commercial
components.
47Handbook Contents
- The Space Radiation Environment
- Radiation Effects Prediction Techniques
- Radiation Effects in Electronic Components
- Designing Tolerant Systems
- Radiation Effects Databases
- Radiation Testing
- Hardness Assurance Management
- Recommended Procurement Practices
48COMRAD-UKExperts Forum
- The Experts Forum allows users to post queries
on the Web-site. - These will, as far as possible, be answered by
Spur Electron but it is also possible for other
users to provide an input and start a discussion.
49 Summary
- COMRAD-UK is a Web based integrated source of
components radiation effects data. - COMRAD-UK is co-sponsored by the British National
Space Centre and maintained on their behalf by
SPUR-Electron. - The site is under continuous development
- - comments and suggestions are welcome.
- comrad-uk.net
- radinfo_at_spurelectron.com
50Hardness Assurance in the real world
- WE HAVENT GOT THE MONEY
- SO WEVE GOT TO THINK.
- (Lord Rutherford 1871-1937)