FLEX

Suppression · CIR / MDCA

FLEX

Flame Extinguishment Experiment

Suppression · CIR / MDCA

Oxygen tested
12–30%
Across 15 extracted test conditions
Pressure
8 settings
0.7 and 1 atmospheric pressures / 1.0 atm / 532.2 mmHg +5 more
Airflow
6 settings
Uox = 10.7 cm/s / Uox = 6.7 cm/s / Quiescent microgravity environment +3 more
Fuel
Liquid
Methane / Methanol / Heptane / Methanol (CH3OH) +1 more

Research brief.

From the NASA challenge brief

Studied fire suppression by diluting the chamber atmosphere with carbon dioxide and helium while burning droplets of liquid fuel.

Objectives stated in the papers

Dynamic Flame Extinguishment

Determine the limiting oxygen index (LOI) for methanol in oxygen-nitrogen-carbon dioxide and oxygen-nitrogen-helium gas mixtures

Develop predictive theoretical and numerical codes and chemical kinetic schemes to model flammability boundaries as a function of effective gravitational acceleration.

AI synthesis.

Across every indexed paper for FLEX

The AI backend isn't connected, so summaries can't be generated right now.

What the experiments revealed.

12 of 17 extracted findings · verified first, then by AI confidence

  1. 01

    The limiting oxygen index (LOI) for methanol in oxygen-nitrogen-carbon dioxide and oxygen-nitrogen-helium diluent gases is approximately 12% to 13% oxygen by volume.

    Prevention · NTRS 20130014061 · p. 1 · AI confidence 95% · Unverified

  2. 02

    The reported flame dimension represents the outer edge of the OH chemiluminescence.

    Detection · NTRS 20150023456 · p. 14 · AI confidence 95% · Unverified

  3. 03

    Flame size measurement is difficult due to dim flames and noise in LLUV images, with window damage exacerbating the issue.

    Detection · NTRS 20150023456 · p. 14 · AI confidence 95% · Unverified

  4. 04

    Methanol burns with a very dim blue flame with small standoff distance and little soot production, unlike heptane.

    Other · NTRS 20090014812 · p. 2 · AI confidence 95% · Unverified

  5. 05

    At high oxygen concentrations, droplets burn to completion rather than exhibiting flame extinction.

    Other · NTRS 20090014812 · p. 2 · AI confidence 95% · Unverified

  6. 06

    Under quasisteady burning assumptions, initial droplet size should not significantly influence the determination of extinction droplet size.

    Other · NTRS 20090014812 · p. 2 · AI confidence 95% · Unverified

  7. 07

    Ambient pressure does not significantly influence droplet burning rate but influences chemistry at sufficiently low values.

    Other · NTRS 20090014812 · p. 2 · AI confidence 95% · Unverified

  8. 08

    The GBEX experiment utilizes a cup burner with a chimney, igniter, and ultrasonic atomizer for oxidizer and agent inlet.

    Other · NTRS 20040142357 · p. 1 · AI confidence 90% · Unverified

  9. 09

    The FSEE experiment setup includes a chimney, cup burner, chamber, PIV-MZI optics, flow modules, and an ultrasonic atomizer.

    Other · NTRS 20040142357 · p. 10 · AI confidence 90% · Unverified

  10. 10

    Direct Numerical Simulation (DNS) for the extinguishment study uses full chemistry (GRI Mech 1.2), radiative loss, and mixture rules.

    Other · NTRS 20040142357 · p. 10 · AI confidence 90% · Unverified

  11. 11

    Water absorption into the methanol droplet during combustion leads to a gradual increase in water concentration; when water mass reaches about 30%, outward water transport begins, lowering the adiabatic flame temperature below the range required for chemical-kinetic gas-phase flame extinguishment.

    Suppression · NTRS 20130014061 · p. 3 · AI confidence 90% · Unverified

  12. 12

    Methanol droplet extinction occurs via two mechanisms: diffusive extinction due to insufficient residence time at the flame, and radiative extinction due to excessive heat loss from the flame zone.

    Suppression · NTRS 20130014061 · p. 1 · AI confidence 90% · Unverified

Read the original research.

The Effect of Pressure on Radiative Losses in Hot, Warm, and Cool Microgravity Spherical Diffusion Flames
2026 · Accepted Manuscript (Version with final changes) · Complete
Space Experiment Concepts: Cup-Burner Flame Extinguishment
2019 · Conference Paper · Complete