FLEX-2

Suppression · CIR / MDCA

FLEX-2

Flame Extinguishment Experiment 2

Suppression · CIR / MDCA

Oxygen tested
12.5–15%
Across 8 extracted test conditions
Pressure
3 settings
0 to 3 atm / 0.7 atm / 1.0 atm
Airflow
2 settings
variable / laminar, axisymmetric
Fuel
Liquid
droplet / solid / gas-jet / methanol +2 more

Research brief.

From the NASA challenge brief

Burned droplets of liquid fuel in the Multi-user Droplet Combustion Apparatus inside the Combustion Integrated Rack.

Objectives stated in the papers

investigates the structure of lifting and lifted flames

study fundamental combustion science problems and other topics of applied combustion research

examining the burning and extinction characteristics of a wide variety of fuel samples in microgravity

investigate the transition to soot emission in gas-jet flames

AI synthesis.

Across every indexed paper for FLEX-2

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

What the experiments revealed.

8 of 8 extracted findings · verified first, then by AI confidence

  1. 01

    Soot control remains one of the major unsolved problems in combustion.

    Other · NTRS 20120017940 · p. 2 · AI confidence 95% · Unverified

  2. 02

    BASS results contribute to the limited database of solid combustion in microgravity and guide strategies for extinguishing accidental fires.

    Suppression · NTRS 20120017940 · p. 3 · AI confidence 95% · Unverified

  3. 03

    BASS tests the hypothesis that materials in microgravity with adequate ventilation burn as well or better than in normal gravity.

    Other · NTRS 20120017940 · p. 3 · AI confidence 95% · Unverified

  4. 04

    The FLEX-2 experiment series aims to measure the extinguishing capability of water mist on premixed flames propagating along a tube in the Space Shuttle's Combustion Module (CM-2).

    Other · NTRS 19990053980 · p. 1 · AI confidence 95% · Unverified

  5. 05

    Water droplets interact with flames through five mechanisms: heat removal via vaporization, oxygen/fuel dilution via volume expansion, radical recombination on droplet surfaces, surface wetting, and radiative barrier formation.

    Suppression · NTRS 19990053980 · p. 1 · AI confidence 95% · Unverified

  6. 06

    Water mist technology is being investigated as a replacement for Halon 1301 due to the latter's high ozone depletion potential and manufacturing ban.

    Prevention · NTRS 19990053980 · p. 1 · AI confidence 95% · Unverified

  7. 07

    Microgravity provides an ideal environment for studying flame-water mist interactions by eliminating gravity-induced droplet depletion, coalescence, and complex flow patterns.

    Other · NTRS 19990053980 · p. 1 · AI confidence 95% · Unverified

  8. 08

    External radiative heat flux can cause materials to ignite and spread faster, while radiative heat transfer loss reduces flammability.

    Prevention · NTRS 20120017940 · p. 3 · AI confidence 90% · Unverified

Read the original research.

Fourth International Microgravity Combustion Workshop
1997 · Conference Proceedings · Complete