Investigations

PSI-69 · FLEX

“The FLEX (Flame Extinguishment Experiment) investigation aims to map the flammability limits of liquid fuels in microgravity environments, measure the effectiveness of various gaseous fire suppressants such as CO2, He, and SF6, and develop reliable predictive models for combustion limits under reduced gravity conditions.” [PSI JSON: objective]

“The FLEX experiments involve igniting and observing the burning behavior of relatively large droplets.” [PSI JSON: approach]

Overview

Objective [text]

The FLEX (Flame Extinguishment Experiment) investigation aims to map the flammability limits of liquid fuels in microgravity environments, measure the effectiveness of various gaseous fire suppressants such as CO2, He, and SF6, and develop reliable predictive models for combustion limits under reduced gravity conditions. The mission seeks to validate and improve simplified models by incorporating detailed chemical reactions, heat transfer, and material movement, using both space-based data and extensive ground-based tests. Key flight experiment goals include obtaining high-resolution measurements of droplet burning rates, flame extinction behavior, heat radiation, soot levels, and temperature profiles, while systematically analyzing the effects of different ambient conditions and suppressant concentrations. These investigations are essential for advancing the fundamental understanding of combustion processes in microgravity and enhancing fire safety protocols for future space missions.

Sourcedata/raw/psi-data/PSI-69/_investigation/PSI-69.json: objective · PSI investigation

Approach [text]

The FLEX experiments involve igniting and observing the burning behavior of relatively large droplets. A primary objective of the experiments is to determine the Limiting Oxygen Index (LOI) as a function of ambient pressure and determine how the presence of a suppressant influences the LOI . The basic outline of the procedure to construct this diagram is as follows: 1. Select the test pressure (0.5 − 1.5 atm) for the LOI tests. 2. Select a smaller droplet size (≈ 3 mm) 3. Select an ambient oxygen mole fraction that, based on ground-based testing, will support droplets burning to completion (as opposed to extinguishing at a finite droplet size). 4. Perform a droplet combustion test. 5. Increase the droplet size or repeat the test (if finite extinction diameter at flame extinction observed). 6. Continue steps 4 and 5 until flame exists for only a short time after ignition (radiative extinction). 7. Continue steps 4 thru 6 at a decreased ambient oxygen mole fraction. 8. Continue step 7 to an ambient oxygen mole fraction where the droplet does not ignite. There were ambient conditions where the extinction droplet sizes at all ambient oxygen mole fractions were too small to either be observed or measured with the available diagnostics. In this case, the determination of the LOI is similar, but more iterative. Instead of observing flame extinction, however, the procedure involved an iterative sequence of tests (burn to completion followed by a no ignition test) with progressively smaller increments in ambient oxygen mole fraction to determine the LOI . For the slow flow tests (in the flight experiment), the configuration of the flight hardware did not allow for adequate diagnostics over the entire test for a droplet in a uniform, steady convective flow. In these tests, the procedure will be to duplicate tests above which yield finite-sized extinction droplet diameters. Near the end of the tests, prior to flame extinction, the droplet will be subjected to a small, sub-buoyant, convective flow (imparted by translating the droplet at a slow, uniform speed). The goal of the experiment is then to see how the presence of this flow influences the extinction process. Note, a large number of the tests involve free droplets (as opposed to fiber-supported droplets) and a number of these tests will have droplets with a slow drift velocity. Data gathered from these tests to examine the influences of a small, sub-buoyant flow on both the burning and extinction process.

Sourcedata/raw/psi-data/PSI-69/_investigation/PSI-69.json: approach · PSI investigation

Hypothesis [text]

The primary hypothesis of the FLEX mission is that microgravity conditions fundamentally alter the combustion and extinction characteristics of liquid fuel droplets due to changes in species and energy transport dynamics, radiative heat loss, and chemical kinetics. Specifically, the hypothesis posits that the lack of buoyant convection in microgravity will lead to significant differences in the flammability limits and suppression efficacy of various fire suppressant agents compared to normal gravity conditions. This hypothesis underpins the design of the FLEX experiments, which aim to map flammability boundaries, quantify suppressant efficacy, and develop predictive models to improve fire safety in space environments.

Sourcedata/raw/psi-data/PSI-69/_investigation/PSI-69.json: hypothesis · PSI investigation

Research impacts [text]

The research impacts and Earth benefits of the FLEX mission are significant and multifaceted. By enhancing our understanding of microgravity combustion, the mission directly contributes to improved fire safety protocols for future space missions, ensuring the safety of crew members in environments where traditional fire suppression methods may be ineffective. On Earth, the insights gained from these experiments have the potential to advance fire safety in confined and reduced-gravity environments, such as submarines or high-altitude aircraft. The mission's findings on the effectiveness of various fire suppressants, including CO2, He, and SF6, in microgravity can lead to the development of more efficient and less harmful fire suppression systems, reducing the risk of toxic byproducts during fire events. Additionally, the study of ''cool flames'' and low-temperature combustion processes observed in microgravity can inform the design of advanced combustion engines, leading to improved fuel efficiency and reduced emissions in automotive and industrial applications. Overall, the FLEX mission's contributions to combustion science have the potential to enhance both space exploration safety and terrestrial fire safety technologies.

Sourcedata/raw/psi-data/PSI-69/_investigation/PSI-69.json: researchImpacts · PSI investigation

Hardware [text]

Combustion Integrated Rack (CIR)-Fluids and Combustion Facility (FCF), Multi-user Droplet Combustion Appartatus (MDCA)

Sourcedata/raw/psi-data/PSI-69/_investigation/PSI-69.json: experimentHardware · PSI investigation

Flight program [text]

International Space Station (ISS)

Sourcedata/raw/psi-data/PSI-69/_investigation/PSI-69.json: flightProgram · PSI investigation

Start date [text]

08-01-2007

Sourcedata/raw/psi-data/PSI-69/_investigation/PSI-69.json: investigationStartDate · PSI investigation

End date [text]

07-31-2016

Sourcedata/raw/psi-data/PSI-69/_investigation/PSI-69.json: investigationEndDate · PSI investigation

Tests

274 tests with extracted table records (SAME-R aging sub-runs grouped by parent ID) · 2096 extracted values (source: data/conditions/PSI-69.csv).

Variation is observed in extracted values; it does not establish the experimental design.

VariableObservedDistinct values / testsRange
diluent [data/conditions/PSI-69.csv]distinct values as recorded2 / 268N2, mixed
droplet_diameter_initial [data/conditions/PSI-69.csv]varied163 / 2621.1 mm – 4.67 mm
fuel [data/conditions/PSI-69.csv]distinct values as recorded2 / 274Heptane, Methanol
o2_mole_fraction [data/conditions/PSI-69.csv]varied15 / 27412.0% – 34.0%
outcome:burn_time [data/conditions/PSI-69.csv]measured162 / 2680.3 s – 39.2 s
outcome:test_end [data/conditions/PSI-69.csv]measured3 / 274Completion, Disruption, Extinction
outcome:visible_flame_extinction_diameter [data/conditions/PSI-69.csv]measured145 / 1970 mm – 4.6 mm
pressure [data/conditions/PSI-69.csv]varied182 / 27370.2 kPa (10.2 psia) – 309 kPa (44.9 psia)

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Additional outcome cells, where available, are displayed as written. Source: data/derived/outcomes_extra.csv.

Instruments mentioned in the approach

No instrument sentence identified in the approach text.

Experimental table columns

Data

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Publications

Data reuse

Not stated in PSI [not in PSI] data/raw/psi-data/PSI-69/_investigation/PSI-69.json: related_glds · PSI investigation

Other PSI records that list this investigation

These are links recorded in PSI; their presence alone does not describe the reuse relationship.

PSI page

PSI page data/manifest/web_check_2026-11-14.csv: line 1 URL pattern

In PYRION

Explore tests · · PSI DOI: 10.60555/mbq8-0451
Enginepyrion-applicability-engine 0.2.0Modedeterministic · no LLM in the verdictDataNASA PSI · 10,299 records used by the engineChecked2026-11-15 09:00 UTCValidation0 critical findings

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