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Brookhaven National Laboratory Tandem Van de Graaff

The Tandem Van de Graaff is the Brookhaven accelerator most of the published planetary single event effect results were taken on. Its distinguishing property for a test planner is that ion energy is tunable at the machine rather than by putting a degrader in the beam, so there is no straggling in the energy distribution reaching the part, and a single event effects campaign can be turned around in a week [2].

Exposures are run in vacuum, and the energies are the lowest of the four accelerators on the radiation testing page: ranges in silicon of 30 to 200 micrometers, so parts are delidded and flip chips thinned, or at the high-LET tune not tested at all [1].

Two other Brookhaven beams are not this facility. The NASA Space Radiation Laboratory runs at energies whose ranges in silicon allow a whole circuit card assembly to be irradiated without delidding; its envelope, its spilled beam structure and the error that structure introduces are recorded on the radiation testing page. The Alternating Gradient Synchrotron was used to deliver 10 GeV per nucleon gold ions at 12 MeV-cm2/mg linear energy transfer at normal incidence, at a range far exceeding that of 200 MeV proton recoils, which was sufficient to latch up any device with a measurable cross section below that LET [6].

ParameterValue
OperatorBrookhaven National Laboratory [2]
LocationUpton, New York, United States
CommissionedNot published
TypeTandem electrostatic accelerator, heavy ion single event effects
Floor areaNot published
CapabilitiesHeavy ion beam line
Simulant or terrainNot applicable
InstrumentationNot published
Ground truthNot published. Test methods follow ASTM F1192 or JEDEC JESD57 [4][5]
Fidelity limitsMonoenergetic single-species beam; 30 to 200 micrometer range in silicon [1]
AccessUser facility. One week campaign turnaround achievable [2]
Cited byradiation testing, sensors and IMUs

No operator-written facility description is held. The envelope below comes from two users’ facility comparisons and from the ion, energy and range figures recorded in the campaigns themselves [1][2][3].

ParameterValue
Working volumeVacuum chamber; dimensions not published [4]
Test article limitsCeramic cover removed; flip chip thinned, or not tested at the high LET tune [1]
VacuumYes. Heavy ion exposures are run in vacuum [4]
TemperatureSet by the user. Campaigns here report room temperature to 90 C [3]
IlluminationNot applicable
SlopeNot applicable
Gravity offloadNot applicable
InstrumentationSupplied by the user

Two tunes. The low-LET tune covers 1 to 6 MeV-cm2/mg at 85 to 200 micrometers of range in silicon, with the ceramic cover removed, flip chips thinned, and no heat spreader or heat sink [1]. The high-LET tune covers 6 to 85 MeV-cm2/mg at 30 to 85 micrometers, and flip-chip parts should not be tested on it at all.

The ranges the campaign records give are consistent with that: bromine-81 at 287 MeV reaches 36 micrometers in silicon at LET 37.5 MeV-cm2/mg at normal incidence, and silicon-28 at 187 MeV reaches 74 micrometers at LET 7.8 [3].

Because ion energy is tunable at the machine, no degrader is needed to reach an intermediate energy, and the beam therefore arrives without the energy spread a degrader introduces [2]. That is what makes a one week turnaround possible.

The spectrum. Monoenergetic, single-species, as at every accelerator here. See the radiation testing page.

Penetration. The shortest ranges of the four facilities, 30 micrometers at the high-LET tune, so every part is opened and many are thinned [1]. A result taken here is a result on a modified part.

A stated envelope. Nothing held is written by the operator. The two tune rows above come from a JPL test-engineering guideline whose author states in its own foreword that the facility table was already out of date at publication [1].

A Van de Graaff was one of four ion source categories in the earliest written JPL heavy ion upset practice, alongside fission fragment sources, alpha emitters and cyclotrons [9]. That guideline carries no device data, and its facility recommendations name the 1984 machines then available to JPL [9]. What still applies here is the equipment it lists for the experimenter to bring: vacuum chamber, beam energy and flux measurement, uniformity measurement, a positioning test card and a device exerciser.

The alternatives differ mainly in penetration and in how fast the ion can be changed.

  • Cyclotron cocktails. The Berkeley 88-Inch Cyclotron offers four cocktails at 4.5 to 30 MeV per nucleon, 1 to 100 MeV-cm2/mg and 40 to 1400 micrometers of range in silicon, and switches species in about two minutes by retuning frequency [8]. Those are operator-stated capabilities, not measurements [8]. The Texas A&M beam is run in air, which the compendia pair with this facility’s vacuum work [4][5].
  • Very high energy beams. The Michigan State facility delivers 60 to 143 MeV per nucleon in air, penetrates commercial package overlayers without delidding, and agreed with Brookhaven results on a Matra HM65656 SRAM [10]. Switching ions takes a 24 hour retune and beam time cost 2300 to 2700 dollars per hour at commissioning. The same paper records a plastic packaged IDT71256 whose cross section was two orders of magnitude below the delidded part on a degraded krypton beam, because the ions ranged out [10]. The NASA Space Radiation Laboratory pursues the same goal with millimeter ranges and a Bragg peak method, which its author states still needs validation across device types and package configurations [7].

The cost of the tandem route is therefore the preparation of the part. Nothing held states a per-hour price or an annual hour budget for this facility.

MEMS accelerometer latchup against temperature, reported 2018. Two Colibrys parts were exposed under bromine-81 and silicon-28 [3]. The SF1600S showed a non-destructive latchup threshold between LET 7.88 and 11.44 MeV-cm2/mg above 70 C at maximum recommended bias, and the MS1002A between 11.44 and 19.71 above 70 C. The temperature dependence is the result worth carrying: on the MS1002A the latchup cross section at LET 37.5 and 1e7 ions/cm2 was 6.1e-6 cm2 at 75 C against 1.5e-6 cm2 at room temperature, a factor of four [3]. A latchup screen run at ambient understates the flight case by that factor for this part.

JPL compendia heavy ion exposures, 2007 to 2012. The vacuum heavy ion half of both JPL compendia was run here, with the in-air and longer-range work at Texas A&M [4][5]. Entries taken in this configuration include the Elpida EDS5104ABTA-75 512 Mbit SDRAM, upsetting above LET 2.7 MeV-cm2/mg, with a recoverable mode-register functional interrupt above 3.8 and a run of over a thousand consecutive errors above 5.4, the latter clearing on rewrite or power cycle [4]. The same part family in the later compendium upset and suffered functional interrupts below LET 2 at about 2e-9 cm2 per bit [5]. The sample size and method caveats that apply to every compendium entry are on the Texas A&M page.

Commercial parts for a Class D payload, reported 2018. Fourteen commercial parts were screened for latchup at this facility and at Texas A&M [3]. Four latch destructively: the LTC2440 ADC, the LTC6655 reference, an ECS 4 MHz crystal oscillator and the Altera EN5322QI regulator, which fails permanently at LET 42.8 MeV-cm2/mg. The method point is range: a 287 MeV bromine beam cannot pass the 12.76 micrometer copper redistribution layer of the DRV8412 motor driver, so a clean result there would have been a false negative, and the authors confirmed stackup by cross sectioning and SEM [3].

Europa Clipper candidate parts, reported 2019. The Applied Physics Laboratory heavy ion work used a 15 MeV per nucleon beam only, with LET coverage stopping at 75 to 83 MeV-cm2/mg, so saturation cross sections above that are extrapolated for most parts [11].

Test conditions that decide whether a result transfers

Section titled “Test conditions that decide whether a result transfers”

Three later works state conditions the screening data above depend on.

Preparation and exercise state. A 2016 JPL tutorial chapter states that heavy ion parts are de-lidded and tested in vacuum because the ion range is tens of micrometers, and that bias and exercise state dominate results for complex devices [12]. On some microprocessors the cross section at a given LET rose by an order of magnitude when the exercising program used the cache [12], so a processor cross section cited without its test program is not a usable number. The chapter is analytical and irradiated no hardware; its worked rate example uses hypothetical parts. It tabulates a typical ion menu from lithium at LET 0.45 to gold at 82.3 MeV-cm2/mg with no facility named [12].

Misdiagnosed mechanisms. The 2019 Europa Clipper characterization of the RH3845 step-down controller used the Berkeley cyclotron and a pulsed laser rather than this machine, but it bears on how any beam result is read [13]. A destructive event first attributed to single event burnout was traced to transient-induced cross conduction in the external synchronous MOSFETs, and raising the in-line gate resistance from 2 to 10 ohms removed it up to 100 V input at LET 79 MeV-cm2/mg. The authors state the root cause is still under investigation and that the effect can occur electrically without a beam, so the beam cross section may measure an instability the beam only triggers. The mitigation was a board-level choice, not a part derating.

Acceptance thresholds. The 2021 NASA radiation hardness assurance guidelines define the categorization framework, the accepted LET acceptance thresholds and what a single event effects test requirement must specify [14]. They contain no measured part results, and the SET signature tables apply only to radiation hardened parts, not commercial ones. The 42.8 MeV-cm2/mg ceiling of the 2018 screen has to be read against those thresholds rather than as a rating [3].

No operator-written description of the machine is held, so commissioning date, floor area, flux range and beam uniformity are unpublished here. The tune ranges rest on a guideline whose author calls its facility table out of date [1]. The campaigns above are screening data on two to three parts per type [3][4][5], and the 2018 screen reports no upset, functional interrupt or dose data and is bounded by an LET of 42.8 MeV-cm2/mg, below the customary 75 to 85 qualification point [3]. Whether a result on a delidded or thinned part transfers to the packaged flight part is not answered by anything held. The facility has not been compared with the others on identical parts beyond the single SRAM agreement reported by Michigan State [10].

References

  1. Guertin, S. M. (2018). Guideline for Single-Event Effect (SEE) Testing of System on a Chip (SOC) Devices . NASA, 20190002148. Source
    BibTeX
    @techreport{guertin2018guideline,
      title = {Guideline for Single-Event Effect (SEE) Testing of System on a Chip (SOC) Devices},
      author = {Guertin, Steven M.},
      number = {20190002148},
      institution = {NASA},
      year = {2018},
      url = {https://ntrs.nasa.gov/citations/20190002148},
      abstract = {The use of complex single and multicore processors with significant cache memory, on-chip peripherals, memory controllers, and high speed input/output (IO) that integrate many of the parts of a traditional computer system is becoming more common in space applications. Such devices are often referred to as system on a chip devices (SOCs), even though the term is used somewhat inaccurately due to the lack of analog and mixed signal subcircuits. These devices are complex combinations of single- or multi-core processors with memory controllers, high-speed input/output (IO), and other peripheral structures that formerly would have been handled by off-chip resources. In the past the processors were tested for single event effects (SEE) separately, and the peripherals were often put into custom application-specific integrated circuits (ASICs) along with other resources required by the user. Performance and cost pressures have pushed commercial devices to incorporate many of the functional blocks into a single chip, an SOC. The NASA Electronic Parts and Packaging Program (NEPP) has been examining ways to perform SEE radiation hardness assurance (RHA) testing of these processor-centric SOCs to achieve reasonable understanding of their performance in space missions.}
    }
  2. Thorbourn, D. (2013). JPL Radiation Effects Facilities . JPL Open Repository. Source
    BibTeX
    @inproceedings{thorbourn2013jpl,
      title = {JPL Radiation Effects Facilities},
      author = {Thorbourn, Dennis},
      booktitle = {JPL Open Repository},
      year = {2013},
      url = {https://dataverse.jpl.nasa.gov/dataset.xhtml?persistentId=hdl:2014/42836}
    }
  3. Daniel, A. C. and Allen, G. R. (2018). Heavy-Ion Test Results of Several Commercial Components for Use in a JPL Class D Interplanetary Mission Payload . JPL Open Repository. Source
    BibTeX
    @inproceedings{daniel2018heavy,
      title = {Heavy-Ion Test Results of Several Commercial Components for Use in a JPL Class D Interplanetary Mission Payload},
      author = {Daniel, Andrew C. and Allen, Gregory R.},
      publisher = {JPL Open Repository},
      year = {2018},
      url = {https://dataverse.jpl.nasa.gov/dataset.xhtml?persistentId=hdl:2014/48478}
    }
  4. McClure, S. S., Allen, G. R., Irom, F., Scheick, L. Z., Adell, P. C. and Miyahira, T. F. (2010). Compendium of test results of recent single event effect tests conducted by the Jet Propulsion Laboratory . IEEE Radiation Effects Data Workshop. Source
    BibTeX
    @inproceedings{mcclure2010compendium,
      title = {Compendium of test results of recent single event effect tests conducted by the Jet Propulsion Laboratory},
      author = {McClure, Steven S. and Allen, Gregory R. and Irom, Farokh and Scheick, Leif Z. and Adell, Philippe C. and Miyahira, Tetsuo F.},
      booktitle = {IEEE Radiation Effects Data Workshop},
      pages = {6-6},
      publisher = {IEEE},
      year = {2010},
      doi = {10.1109/redw.2010.5619495},
      abstract = {This paper reports heavy ion and proton-induced single event effect (SEE) results from recent tests for a variety of microelectronic devices. The compendium covers devices tested over the last two years by the Jet Propulsion Laboratory.}
    }
  5. Allen, G. R., Guertin, S. M., Scheick, L. Z., Irom, F. and Zajac, S. (2012). Compendium of recent test results of single event effects conducted by the Jet Propulsion Laboratory . IEEE Radiation Effects Data Workshop. Source
    BibTeX
    @inproceedings{allen2012compendium,
      title = {Compendium of recent test results of single event effects conducted by the Jet Propulsion Laboratory},
      author = {Allen, Gregory R. and Guertin, Steven M. and Scheick, Leif Z. and Irom, Farokh and Zajac, Stephanie},
      booktitle = {IEEE Radiation Effects Data Workshop},
      pages = {1-10},
      publisher = {IEEE},
      year = {2012},
      doi = {10.1109/redw.2012.6353747},
      abstract = {This paper reports heavy ion, proton, and laser induced single event effects results for a variety of microelectronic devices targeted for possible use in NASA spacecrafts. The compendium covers devices tested within the years of 2010 through 2012.}
    }
  6. Reddell, B. D. (1999). Orbiter Avionics Radiation Handbook . NASA, 20180002644. Source
    BibTeX
    @techreport{reddell1999orbiter,
      title = {Orbiter Avionics Radiation Handbook},
      author = {Reddell, Brandon D.},
      number = {20180002644},
      institution = {NASA},
      year = {1999},
      url = {https://ntrs.nasa.gov/citations/20180002644},
      abstract = {This handbook was assembled to document he radiation environment for design of Orbiter avionics. It also maps the environment through vehicle shielding and mission usage into discrete requirements such as total dose. Some details of analytical techniques for calculating radiation effects are provided. It is anticipated that appropriate portions of this document will be added to formal program specifications. }
    }
  7. Irom, F. (2023). Standardizing NASA’s Approach to Using High-Energy Heavy Ions for SEE Assurance. doi.org/10.48577/jpl.bv6gxz
    BibTeX
    @misc{irom2023standardizing,
      title = {Standardizing NASA’s Approach to Using High-Energy Heavy Ions for SEE Assurance},
      author = {Irom, Farokh},
      howpublished = {Presentation at the JPL Open Repository},
      year = {2023},
      doi = {10.48577/jpl.bv6gxz}
    }
  8. Covo, M. K., Albright, R. A., Ninemire, B., Johnson, M., Hodgkinson, A., Loew, T., Benitez, J. Y., Todd, D. S., Xie, D., Perry, T., Phair, L., Bernstein, L. A., Bevins, J. E., Brown, J. A., Goldblum, B. L., Harasty, M. D., Harrig, K., Laplace, T. A., Matthews, E. F., Bushmaker, A., Walker, D., Oklejas, V., Hopkins, A. R., Bleuel, D. L., Chen, J. and Cronin, S. B. (2017). The 88-Inch Cyclotron: A one-stop facility for electronics radiation and detector testing . Measurement. Source
    BibTeX
    @article{covo2017inch,
      title = {The 88-Inch Cyclotron: A one-stop facility for electronics radiation and detector testing},
      author = {Covo, M. Kireeff and Albright, Robert A. and Ninemire, B. and Johnson, Michael and Hodgkinson, A. and Loew, T. and Benitez, J. Y. and Todd, D. S. and Xie, D.Z. and Perry, T. and Phair, L. and Bernstein, L. A. and Bevins, James E. and Brown, J. A. and Goldblum, B. L. and Harasty, M. D. and Harrig, K.P. and Laplace, T. A. and Matthews, E. F. and Bushmaker, Adam and Walker, David and Oklejas, Vanessa and Hopkins, Alan R. and Bleuel, D. L. and Chen, J. and Cronin, Stephen B.},
      journal = {Measurement},
      volume = {127},
      pages = {580-587},
      publisher = {Elsevier BV},
      year = {2017},
      doi = {10.1016/j.measurement.2017.10.018}
    }
  9. Nichols, D. K., Price, W. E. and Malone, C. (1984). A Guideline for Heavy Ion Radiation Testing for Single Event Upset (SEU) . Jet Propulsion Laboratory, California Institute of Technology, JPL Publication 84-22. Source
    BibTeX
    @techreport{nichols1984guideline,
      title = {A Guideline for Heavy Ion Radiation Testing for Single Event Upset (SEU)},
      author = {Nichols, Donald K. and Price, William E. and Malone, Carl},
      number = {JPL Publication 84-22},
      institution = {Jet Propulsion Laboratory, California Institute of Technology},
      year = {1984},
      url = {https://ntrs.nasa.gov/citations/19840020507},
      abstract = {A guideline for heavy ion radiation testing for single event upset was prepared to assist new experimenters in preparing and directing tests. How to estimate parts vulnerability and select an irradiation facility is described. A broad brush description of JPL equipment is given, certain necessary pre-test procedures are outlined and the roles and testing guidelines for on-site test personnel are indicated. Detailed descriptions of equipment needed to interface with JPL test crew and equipment are not provided, nor does it meet the more generalized and broader requirements of a MIL-STD document. A detailed equipment description is available upon request, and a MIL-STD document is in the early stages of preparation.}
    }
  10. Ladbury, R., Reed, R. A., Marshall, P. W., LaBel, K. A., Anantaraman, R., Fox, R., Sanderson, D. P., Stolz, A., Yurkon, J., Zeller, A. F. and Stetson, J. W. (2004). Performance of the High-Energy Single-Event Effects Test Facility (SEETF) at Michigan State University's National Superconducting Cyclotron Laboratory (NSCL) . IEEE Transactions on Nuclear Science, 20040171458. Source
    BibTeX
    @article{ladbury2004performance,
      title = {Performance of the High-Energy Single-Event Effects Test Facility (SEETF) at Michigan State University's National Superconducting Cyclotron Laboratory (NSCL)},
      author = {Ladbury, R. and Reed, R. A. and Marshall, Paul W. and LaBel, Kenneth A. and Anantaraman, R. and Fox, R. and Sanderson, D. P. and Stolz, A. and Yurkon, J. and Zeller, A. F. and Stetson, J. W.},
      journal = {IEEE Transactions on Nuclear Science},
      volume = {51},
      number = {20040171458},
      pages = {3664-3668},
      institution = {NASA},
      address = {Atlanta, Georgia},
      year = {2004},
      doi = {10.1109/tns.2004.839300},
      abstract = {The performance of Michigan State University's Single-Event Effects Test Facility (SEETF) during its inaugural runs is evaluated. Beam profiles and other diagnostics are presented, and prospects for future development and testing are discussed.}
    }
  11. Pham, C. H., Caughran, D. F. and Likar, J. J. (2019). Compendium of Recent Radiation Test Results from the Johns Hopkins University Applied Physics Laboratory . IEEE Radiation Effects Data Workshop. Source
    BibTeX
    @inproceedings{pham2019compendium,
      title = {Compendium of Recent Radiation Test Results from the Johns Hopkins University Applied Physics Laboratory},
      author = {Pham, Chi H. and Caughran, Daniel F. and Likar, Justin J.},
      booktitle = {IEEE Radiation Effects Data Workshop},
      pages = {1-8},
      publisher = {IEEE},
      year = {2019},
      doi = {10.1109/redw.2019.8906564},
      abstract = {Total Ionizing Dose (TID), Enhanced Low Dose Rate Sensitivity (ELDRS), and Single Event Effect (SEE) test results are presented for a variety of analog, digital, mixed signal, and Radio Frequency (RF) devices.}
    }
  12. Perez, R. J. (2016). Analysis and Simulations of Space Radiation Induced Single Event Effects and Transients . IEEE International Conference on Space Mission Challenges for Information Technology. Source
    BibTeX
    @inproceedings{perez2016analysis,
      title = {Analysis and Simulations of Space Radiation Induced Single Event Effects and Transients},
      author = {Perez, Reinaldo J.},
      booktitle = {IEEE International Conference on Space Mission Challenges for Information Technology},
      publisher = {JPL Open Repository},
      year = {2016},
      url = {https://dataverse.jpl.nasa.gov/dataset.xhtml?persistentId=hdl:2014/49065}
    }
  13. Bozovich, A. N., Barchowsky, A., Allen, G. R., Vartanian, S., Kahn, B. R., Zajac, S. A., Nguyen, D. and Merida, E. W. (2019). Single Event Effects (SEE) and Total Ionizing Dose (TID) test results for a step-down regulator controller evaluated for use in a harsh space radiation environment . AIAA SciTech. Source
    BibTeX
    @inproceedings{bozovich2019single,
      title = {Single Event Effects (SEE) and Total Ionizing Dose (TID) test results for a step-down regulator controller evaluated for use in a harsh space radiation environment},
      author = {Bozovich, Amanda N. and Barchowsky, Ansel and Allen, Gregory R. and Vartanian, Sergeh and Kahn, Branden R. and Zajac, Stephanie A. and Nguyen, Duc and Merida, Elvis W.},
      booktitle = {AIAA SciTech},
      publisher = {JPL Open Repository},
      year = {2019},
      url = {https://dataverse.jpl.nasa.gov/dataset.xhtml?persistentId=hdl:2014/51470}
    }
  14. Hodson, R. F., Pellish, J. A., Austin, R. A., Campola, M. J., Ladbury, R. L., LaBel, K. A., Allen, G. R., Gaza, R. and Willis, E. M. (2021). Avionics Radiation Hardness Assurance (RHA) Guidelines . NASA, NASA/TM-20210018053. Source
    BibTeX
    @techreport{hodson2021avionics,
      title = {Avionics Radiation Hardness Assurance (RHA) Guidelines},
      author = {Hodson, Robert F. and Pellish, Jonathan A. and Austin, Rebekah A. and Campola, Michael J. and Ladbury, Raymond L. and LaBel, Kenneth A. and Allen, Gregory R. and Gaza, Razvan and Willis, Emily M.},
      number = {NASA/TM-20210018053},
      institution = {NASA},
      year = {2021},
      url = {https://ntrs.nasa.gov/citations/20210018053},
      abstract = {Based on the need to develop and adopt timely and up-to-date guidance to ensure that natural space radiation environment threats do not compromise mission success, the NASA Engineering and Safety Center (NESC) was solicited to develop and publish guidance for deriving radiation hardness assurance (RHA) requirements and for evaluating avionics hardware elements with respect to total ionizing dose, total non-ionizing dose, and single event effects. This document contains the outcome of the NESC assessment.}
    }