Investigations

PSI-159 · ACME CFI-G

“Plan and support flight testing on the International Space Station (ISS).” [PSI JSON: objective]

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

Overview

Objective [text]

1. Plan and support flight testing on the International Space Station (ISS). 2. Determine the conditions for which cool diffusion flames occur for propane, n-butane, and n-pentane; normal and inverse flames; and a broad range of Zst, Tad, and fluent flow rate. 3. Support the flight tests with advanced CFD simulations. 4. Identify or develop a chemical kinetics mechanism that yields good agreement between the CFD predictions and the ISS measurements. 5. Disseminate the results as widely as possible.

Sourcedata/raw/psi-data/PSI-159/_investigation/PSI-159.json: objective · PSI investigation

Approach [text]

Perform spherical diffusion flame tests aboard the International Space Station. Consider multiple fuels, a 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-159/_investigation/PSI-159.json: approach · PSI investigation

Hypothesis [text]

The hypotheses of this research are that testing aboard the ISS can demonstrate the following for the first time, contributing to an improved understanding of cool flame kinetics. 1. Steady-state cool diffusion flames on spherical porous burners. 2. Cool diffusion flames burning propane, n-butane, and n-pentane. 3. Cool diffusion flames for a wide range of Zst, Tad, and pressures. 4. Inverse cool diffusion flames. 5. Cool diffusion flames for which a decrease in fluent flow rate will cause extinction, whereas an increase will cause a transition to a hot diffusion flame, with oscillation possible between hot and cool flames.

Sourcedata/raw/psi-data/PSI-159/_investigation/PSI-159.json: hypothesis · PSI investigation

Research impacts [text]

Combustion provides 86% of the world’s energy and an even higher fraction of the energy used for transportation. The internal combustion engines used for transportation generally have thermal efficiencies of 38% or lower because of thermal losses. These efficiencies may increase to 60% if future engines can take advantage of ultra-lean combustion. However, this progress is being impeded by the limited understanding of the chemistry of cool flames. Research into cool diffusion flames (whose peak temperatures are 500 – 1000 K) has grown exponentially since they were discovered in 2012. The measurements performed for this project will help to test and advance cool flame kinetics mechanisms. This should facilitate the development of more efficient internal combustion engines.

Sourcedata/raw/psi-data/PSI-159/_investigation/PSI-159.json: researchImpacts · PSI investigation

Hardware [text]

ACME, Combustion Integrated Rack (CIR)

Sourcedata/raw/psi-data/PSI-159/_investigation/PSI-159.json: experimentHardware · PSI investigation

Flight program [text]

International Space Station (ISS)

Sourcedata/raw/psi-data/PSI-159/_investigation/PSI-159.json: flightProgram · PSI investigation

Start date [not in PSI]

Not stated in PSI

Sourcedata/raw/psi-data/PSI-159/_investigation/PSI-159.json: investigationStartDate · PSI investigation

End date [not in PSI]

Not stated in PSI

Sourcedata/raw/psi-data/PSI-159/_investigation/PSI-159.json: investigationEndDate · PSI investigation

Tests

333 tests with extracted table records (SAME-R aging sub-runs grouped by parent ID) · 2188 extracted values (source: data/conditions/PSI-159.csv).

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

VariableObservedDistinct values / testsRange
burner_o2_mole_fraction [data/conditions/PSI-159.csv]varied12 / 15412.0% – 85.0%
flame_type [data/conditions/PSI-159.csv]distinct values as recorded2 / 333inverse, normal
fuel [data/conditions/PSI-159.csv]distinct values as recorded7 / 33330% butane, 30% ethane, 30% propane, 50% butane, butane, ethane, propane
o2_mole_fraction [data/conditions/PSI-159.csv]varied139 / 17918.0% – 40.0%
outcome:burn_time [data/conditions/PSI-159.csv]measured100 / 3290 s – 304 s
outcome:cool_flame [data/conditions/PSI-159.csv]measured8 / 8no, PCI-hot, yes, PCI-A, yes, PCI-B, yes, PCI-C, yes, PCI-D, yes, PCI-E, yes, PCI-F, yes, PCI-G
outcome:hot_ignition [data/conditions/PSI-159.csv]measured5 / 333No, Yes, flash, no, yes
outcome:o2_mole_fraction_after_test [data/conditions/PSI-159.csv]measured136 / 1790.17939183 1 – 0.397258964 1
pressure [data/conditions/PSI-159.csv]varied11 / 33349.5 kPa (7.18 psia) – 331 kPa (48 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-159/_investigation/PSI-159.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/cyt1-kh64

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