SEECA Workbench

Help & User Guide

Disclaimer: This tool and its accompanying documentation are provided for preliminary analysis and educational purposes only. Results have not been independently verified or validated for use in mission-critical decisions. Users are solely responsible for verifying all outputs against their own analysis and applicable standards before making any design, test, or mission decisions. Space RHA LLC makes no warranties, express or implied, regarding the accuracy, completeness, or fitness for any particular purpose of the results produced by this tool, and shall not be held liable for any damages arising from its use.

1. What this tool does

It runs a single event effect criticality analysis as a worklist. You describe the mission (phases, environments, duration, fleet, risk posture), then one row per function, part and effect mode: what the effect does locally, how it propagates, what the system consequence is, what mitigations are credited, and what evidence exists for the rate. The workbench derives the criticality class, converts the mission requirement into a tolerable rate or a probability budget, predicts the rate in the nominal and worst case environments, grades the evidence, reports a status and a margin, flags the worst case exposure, writes the test a null result would have to show to close an open row, draws the assurance argument, and exports the whole thing as a Markdown report, a CSV worksheet and a JSON file you can reload.

The method: the function level criticality classes of the public NASA SEECA guidance (1996) and its 2020 and 2021 restatements, with tolerable rates from availability, interval or count requirements, destructive effects as probability budgets, and rates from a Weibull against the site environments, a directly entered rate, or a bound from a null result. The methodology section on the tool page explains the why behind each step.

2. A ten minute walk through

  1. Pick a preset. The COTS camera preset is a published case study whose nominal rate the engine reproduces; the smallsat preset shows every class and every status. Or start empty.
  2. Set the mission frame. Duration, number of vehicles, whether a critical loss anywhere in the fleet counts against the budget, the probability budget for critical functions, and how much wider a margin weak evidence must show. The risk posture selector fills these with editable starting points; they are this site's illustrations, not values from a standard.
  3. Define the phases. Each phase has a fraction of mission time, a nominal environment, a worst case environment and a default availability. A row can be active in any subset of phases.
  4. Add rows. One per function, part and mode. Fill the function first: it is the thing the system loses. Then the part, the mode, the local effect, the propagation and the consequence. Pick the consequence from the list; the class depends on it.
  5. Credit mitigations. Tick what the design actually has. Each one changes the model and adds a verification note to the open items.
  6. Enter the evidence. A Weibull per device, a rate you computed elsewhere, or a null result. Choose the grade honestly. The reference field is for the report.
  7. Read the row panel and the summary. Then the open items: each says what would close it.
  8. Export. Download the Markdown report and the JSON. Save in the browser if you want to come back.

3. Inputs, and what they do

4. Reading the output

5. Caveats

6. References

LaBel, Gates, Barth, Johnston and Marshall, Single Event Effect Criticality Analysis, NASA HQ Code QW, 1996. · Campola, Guidance for Implementation of a SEECA, SEE Symposium and MAPLD, 2020, NTRS 20205007785. · Campola and others, Single-Event Transient Case Study for System-Level Radiation Effects Analysis, IEEE Transactions on Nuclear Science, 2021. · NASA/TM-20210018053, Avionics Radiation Hardness Assurance Guidelines, 2021. · Tylka and others, CREME96, IEEE Transactions on Nuclear Science 44(6), 1997. · GSN Community Standard Version 2, SCSC-141B, 2018. · MIL-STD-1629A. · ECSS-Q-ST-30-02C. · ECSS-Q-ST-60-15C.

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