Method and data
FireSight ranks findings with a fixed formula. The same atmosphere always gives the same order, and no language model takes part in the ranking.
How findings are ranked
You choose an atmosphere: oxygen O, pressure P and airflow F. Each finding has its own test conditions o, p and f.
closeness = 1 − mean( |O−o| / 70, |P−p| / 101, |F−f| / 50 )
conditions the source does not report are skipped
relevance = safety relevance (1, 2 or 3) / 3
completeness = reported conditions / 3
score = closeness × relevance × completenessThe divisors are the width of each axis: 70 % O₂, 101 kPa and 50 cm/s. A finding that leaves out a condition is never dropped and never given a guessed value. It loses score through completeness and its card says “not reported”.
This formula is our own design for this tool, not a published NASA method. It is simple on purpose so that every score can be checked by hand.
Worked example
Atmosphere: exploration atmosphere, 34 % O₂, 56.5 kPa, 15 cm/s. Finding: saffire-005, Cotton-fiberglass fabric (SIBAL).
oxygen 1 − |34 − 31| / 70 = 0.957 (% O₂) pressure 1 − |56.5 − 54.1| / 101 = 0.976 (kPa) airflow 1 − |15 − 20| / 50 = 0.900 (cm/s) closeness 0.944 relevance 3 / 3 = 1.000 completeness 3 / 3 = 1.000 score 0.944
Safety relevance
Each finding carries a relevance tag set when the dataset was built:
- 3: directly informs material flammability or extinguishment.
- 2: informs detection or flame behaviour.
- 1: fundamental combustion science.
Tested, thin and untested
A finding is in close range of a point when it reports both oxygen and pressure and lies within ±5 % O₂ and ±15 kPa of it. Findings taken from the same burn share one oxygen and pressure pair, so they count as one test condition.
- Tested: 3 or more test conditions in close range.
- Thin: 1 or 2.
- Untested: none.
The same rule gives the verdict for your atmosphere, the hatching on the chart and the gaps panel. For the ISS cabin preset it returns tested: 3 findings from 3 test conditions. For the exploration preset it returns thin: 4 findings from 2 test conditions. A gap is not evidence of safety. It means this dataset holds no source-checked finding there.
Data rules
- A missing value is shown as “not reported”. It is never guessed.
- A finding appears only after every value was compared with its cited source document. This check was AI-assisted. Independent human review of each row is tracked separately and is not yet complete; the Verify panel shows the status of each finding.
- A flow direction the source does not state is shown as not reported.
- Every card links to its source document and names where in it to look.
How AI is used
- AI helped extract values from NASA documents into the dataset and wrote the investigation summaries and the safety implications for the two preset atmospheres.
- AI-written text is marked with a violet border and the label “AI-generated from NASA PSI records”.
- Each implication cites finding ids. One that cites a finding outside the ranked evidence on screen is not shown. With fewer than 3 cited findings the panel says “Insufficient evidence”.
- The ranking, the coverage verdict, the chart and the gaps use no AI. With every language model switched off they are unchanged.
Limits
- Not a combustion simulator or a predictive model.
- Not a certified safety tool or a source of design limits.
- Not a replacement for NASA's PSI repository. It is a way into it.
- The dataset is small: 28 findings from 7 investigations, of which 11 report both oxygen and pressure.
Data: NASA investigations used
- Burning and Suppression of Solids-II6 findings
BASS-II, ISS, Microgravity Science Glovebox, 2014–2016
Study ignition, flame growth, flame spread and extinction limits of solid fuels burning in low-velocity forced flows in microgravity, with oxygen lowered by nitrogen dilution of the glovebox.
- Burning and Suppression of Solids-II (BASS-II) Summary Report 2021
- Combustion of Solids in Microgravity: Results from the BASS-II Experiment 2016
- Opposed flame spread over PMMA cylinders in microgravity and normal gravity (Scientific Reports) 2018
- Flammability Limits from BASS-II Testing in Microgravity Compared to Normal Gravity Limits (ICES-2019) 2019
Saffire, Cygnus cargo vehicle (uncrewed, after ISS departure), Saffire Flow Unit + Far Field Diagnostics, 2016–2023
Observe large-scale fire growth and spread on thin and thick solid fuels in long-duration microgravity, including the reduced-pressure, elevated-oxygen atmospheres planned for exploration spacecraft, and measure the fire's impact on the vehicle.
SoFIE-MIST, ISS, Combustion Integrated Rack (SoFIE insert), 2023–2025
Map ignition and extinction boundaries of PMMA cylinders as a function of flow speed, oxygen concentration, pressure and external radiant heating, with emphasis on NASA's proposed space exploration atmospheres.
- Flame Extinguishment Experiment (FLEX)3 findings
FLEX, ISS, Combustion Integrated Rack (Multi-User Droplet Combustion Apparatus), 2009–2012
Study how isolated burning fuel droplets extinguish in microgravity across oxygen levels, pressures and diluents (nitrogen, carbon dioxide, helium), to inform fire suppression for spacecraft.
- ACME – Burning Rate Emulator (BRE)4 findings
ACME-BRE, ISS, Combustion Integrated Rack (ACME insert), 2019–2020
Use a gas-fed porous burner with embedded heat-flux gauges to emulate the burning of solid and liquid materials, and map which materials can burn steadily in microgravity at different oxygen levels and pressures.
CFI-G, ISS, Combustion Integrated Rack (ACME insert), 2021
Produce and study steady, spherical non-premixed cool flames burning gaseous fuel in microgravity, without the heated reactants ground tests require.
SLICE, ISS, Microgravity Science Glovebox, 2012
Measure the shape, liftoff, stability and soot of laminar coflow methane jet flames in microgravity and normal gravity to test combustion models.