Investigations

PSI-10 · ACME/Flame Design

“Obtain soot-inception limits of quasi-steady normal and inverse spherical diffusion flames as functions of flow rate, Zst, amount of inert (N2 or CO2), and pressure for C2H4 and CH4 flames.” [PSI JSON: objective]

“Perform spherical diffusion flame tests in drop towers and aboard the International Space Station.” [PSI JSON: approach]

Overview

Objective [text]

The primary objectives of this flight experiment are: A. Obtain soot-inception limits of quasi-steady normal and inverse spherical diffusion flames as functions of flow rate, Zst, amount of inert (N2 or CO2), and pressure for C2H4 and CH4 flames. Identify the corresponding temperatures in hot regions. Obtain similar limits and temperatures for inverse and normal coflow flames. B. Obtain detailed measurements in quasi-steady normal and inverse spherical diffusion flames for C2H4 and CH4. Determine the effects of flow rate, Zst, amount of N2, and pressure on flame temperature, size, color, and soot volume fraction. Evaluate the possible existence of steady flames. C. Obtain extinction limits as functions of Zst, amount of N2, and pressure for normal and inverse spherical C2H4 and CH4 flames. Identify the corresponding temperatures in hot regions. Identify the presence of radiative or kinetic extinction. Evaluate whether pseudo-flammability limits can be obtained for these flames.

Sourcedata/raw/psi-data/PSI-10/_investigation/PSI-10.json: objective · PSI investigation

Approach [text]

Perform spherical diffusion flame tests in drop towers and aboard the International Space Station. Consider a broad range of reactant dilutions, flow rates and pressures for normal and inverse convection directions. Observe the flames with a broad suite of cameras, radiometers, photomultiplier tubes, and thermocouples.

Sourcedata/raw/psi-data/PSI-10/_investigation/PSI-10.json: approach · PSI investigation

Hypothesis [text]

1. Soot formation requires a region where local C/O ratio and T exceed their critical values, and where strain rate is sufficiently low. 2. Microgravity spherical diffusion flames extinguish when the peak temperature first decreases below 1130 K. 3. Steady-state spherical diffusion flames are possible.

Sourcedata/raw/psi-data/PSI-10/_investigation/PSI-10.json: hypothesis · PSI investigation

Research impacts [text]

This project has the potential for improving efficiency and reducing pollutant emissions in terrestrial combustors. For example, it is contributing to novel designs of future coal power plants.

Sourcedata/raw/psi-data/PSI-10/_investigation/PSI-10.json: researchImpacts · PSI investigation

Hardware [text]

Advanced Combustion via Microgravity Experiments (ACME), Combustion Integrated Rack (CIR), Reconfiguration of Combustion Integrated Rack (CIR)

Sourcedata/raw/psi-data/PSI-10/_investigation/PSI-10.json: experimentHardware · PSI investigation

Flight program [text]

International Space Station (ISS)

Sourcedata/raw/psi-data/PSI-10/_investigation/PSI-10.json: flightProgram · PSI investigation

Start date [text]

01-14-1999

Sourcedata/raw/psi-data/PSI-10/_investigation/PSI-10.json: investigationStartDate · PSI investigation

End date [text]

04-30-2025

Sourcedata/raw/psi-data/PSI-10/_investigation/PSI-10.json: investigationEndDate · PSI investigation

Tests

327 tests with extracted table records (SAME-R aging sub-runs grouped by parent ID) · 2165 extracted values (source: data/conditions/PSI-10.csv).

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

VariableObservedDistinct values / testsRange
burner_o2_mole_fraction [data/conditions/PSI-10.csv]varied58 / 10921.2% – 85.0%
diluent [data/conditions/PSI-10.csv]observed constant1 / 327N2
flame_type [data/conditions/PSI-10.csv]distinct values as recorded2 / 327inverse, normal
fuel [data/conditions/PSI-10.csv]distinct values as recorded3 / 327C2H4, C3H8, ethylene
fuel_phase [data/conditions/PSI-10.csv]observed constant1 / 28gas
o2_mole_fraction [data/conditions/PSI-10.csv]varied188 / 20719.8% – 40.0%
outcome:o2_mole_fraction_after_test [data/conditions/PSI-10.csv]measured187 / 1870.197475265 1 – 0.397248069 1
outcome:pressure_after_test [data/conditions/PSI-10.csv]measured140 / 30743.2991 kPa – 306.886 kPa
pressure [data/conditions/PSI-10.csv]varied129 / 32743 kPa (6.24 psia) – 305 kPa (44.2 psia)

Loading test data…

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

Download extracted data

Publications

Data reuse

Not stated in PSI [not in PSI] data/raw/psi-data/PSI-10/_investigation/PSI-10.json: related_glds · PSI investigation

PSI page

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

In PYRION

Explore tests · · PSI DOI: 10.60555/w4zy-bt45

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