Materials and oxygen

Ambient oxygen ceilings

Phase is taken from the test, or from the investigation-wide record when it has exactly one extracted phase. Missing or ambiguous phases are excluded. These observations are not design limits.

gas

PSI-10: 40.0% · 20 source records

Show test IDs and sources

21301A1 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=188;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301A2 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=189;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301A3 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=190;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301A4 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=191;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301A5 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=192;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301A6 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=193;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301A7 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=198;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301A8 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=199;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301A9 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=200;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301C1 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=194;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301C2 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=195;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301D1 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=196;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301D2 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=197;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301H1 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=201;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301H2 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=202;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301H3 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=203;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301J1 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=204;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301J2 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=205;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301J3 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=206;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

21301J4 · gravity: microgravity

Source

psi-data/PSI-10/Experimental table/PSI-10_Experimental table_Flame Design_Normal Flame.csv · row=207;column=XO2 (init) · XO2 (init) · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=42 · Flame Design is one of six independent experiments that are part of the ACME project, which used a single modular set of hardware to carry out studies of flames burning gaseous fuels in the ISS’ Combustion Integrated Rack (CIR). · extracted · PSI investigation

Source

psi-data/PSI-10/Reports/PSI-10_Reports_FinalRpt_ACMEFlameDesign.pdf · page=44 · The challenges of normal-gravity studies are avoided by performing the tests on the International Space Station (ISS), where the non-buoyant microgravity flames allow the effects of convection direction and flame structure to be independently varied. · extracted · PSI investigation

PSI-20: 40.0% · 10 source records

Show test IDs and sources

2019-Feb-25 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=3;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

2019-Feb-8 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=1;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

2019-March-4 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=4;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

2020-Dec-11 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=14;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

2020-Dec-17 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=15;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

2020-Dec-23 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=16;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

2020-Dec-4 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=13;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

2020-Dec-5 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=12;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

2020-Sept-3 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=10;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

2021-Jan-28 · gravity: microgravity

Source

psi-data/PSI-20/Experimental table/PSI-20_Experimental table_ACME BRE.csv · row=18;column=Oxygen Conc (percent) · Oxygen Conc (percent) · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=subResearchArea · Flames of Gaseous Fuels · extracted · PSI investigation

Source

psi-data/PSI-20/_investigation/PSI-20.json · section=researchImpacts · Quasi-steady burning corresponding to various condensed-phase materials (such as PMMA and Nylon) was observed in microgravity despite the absence of air flow, where the cessation of ventilation is an established step in putting out spacecraft fires. · extracted · PSI investigation

liquid

PSI-69: 34.0% · 9 source records

Show test IDs and sources

192F001 · gravity: microgravity

Source

psi-data/PSI-69/Experimental table/PSI-69_Experimental table_FLEX.csv · row=20;column=O initial ambient composition; mole fraction · O initial ambient composition; mole fraction · extracted · PSI investigation

Source

psi-data/PSI-69/_investigation/PSI-69.json · section=objective · 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. · extracted · PSI investigation

Source

nasa/iss-combustion-guide-2015/np-2015-10-034-jsc_combustion_in_reduced_gravity-iss-mini-book-011116-508.pdf · page=36 · FLEX and the follow-on FLEX–2 experiments are exploiting the microgravity environment to study the spherically symmetric combustion of liquid droplets. · extracted · PSI investigation

192F002 · gravity: microgravity

Source

psi-data/PSI-69/Experimental table/PSI-69_Experimental table_FLEX.csv · row=21;column=O initial ambient composition; mole fraction · O initial ambient composition; mole fraction · extracted · PSI investigation

Source

psi-data/PSI-69/_investigation/PSI-69.json · section=objective · 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. · extracted · PSI investigation

Source

nasa/iss-combustion-guide-2015/np-2015-10-034-jsc_combustion_in_reduced_gravity-iss-mini-book-011116-508.pdf · page=36 · FLEX and the follow-on FLEX–2 experiments are exploiting the microgravity environment to study the spherically symmetric combustion of liquid droplets. · extracted · PSI investigation

192F003 · gravity: microgravity

Source

psi-data/PSI-69/Experimental table/PSI-69_Experimental table_FLEX.csv · row=22;column=O initial ambient composition; mole fraction · O initial ambient composition; mole fraction · extracted · PSI investigation

Source

psi-data/PSI-69/_investigation/PSI-69.json · section=objective · 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. · extracted · PSI investigation

Source

nasa/iss-combustion-guide-2015/np-2015-10-034-jsc_combustion_in_reduced_gravity-iss-mini-book-011116-508.pdf · page=36 · FLEX and the follow-on FLEX–2 experiments are exploiting the microgravity environment to study the spherically symmetric combustion of liquid droplets. · extracted · PSI investigation

196F001 · gravity: microgravity

Source

psi-data/PSI-69/Experimental table/PSI-69_Experimental table_FLEX.csv · row=19;column=O initial ambient composition; mole fraction · O initial ambient composition; mole fraction · extracted · PSI investigation

Source

psi-data/PSI-69/_investigation/PSI-69.json · section=objective · 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. · extracted · PSI investigation

Source

nasa/iss-combustion-guide-2015/np-2015-10-034-jsc_combustion_in_reduced_gravity-iss-mini-book-011116-508.pdf · page=36 · FLEX and the follow-on FLEX–2 experiments are exploiting the microgravity environment to study the spherically symmetric combustion of liquid droplets. · extracted · PSI investigation

196F002 · gravity: microgravity

Source

psi-data/PSI-69/Experimental table/PSI-69_Experimental table_FLEX.csv · row=23;column=O initial ambient composition; mole fraction · O initial ambient composition; mole fraction · extracted · PSI investigation

Source

psi-data/PSI-69/_investigation/PSI-69.json · section=objective · 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. · extracted · PSI investigation

Source

nasa/iss-combustion-guide-2015/np-2015-10-034-jsc_combustion_in_reduced_gravity-iss-mini-book-011116-508.pdf · page=36 · FLEX and the follow-on FLEX–2 experiments are exploiting the microgravity environment to study the spherically symmetric combustion of liquid droplets. · extracted · PSI investigation

196F003 · gravity: microgravity

Source

psi-data/PSI-69/Experimental table/PSI-69_Experimental table_FLEX.csv · row=24;column=O initial ambient composition; mole fraction · O initial ambient composition; mole fraction · extracted · PSI investigation

Source

psi-data/PSI-69/_investigation/PSI-69.json · section=objective · 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. · extracted · PSI investigation

Source

nasa/iss-combustion-guide-2015/np-2015-10-034-jsc_combustion_in_reduced_gravity-iss-mini-book-011116-508.pdf · page=36 · FLEX and the follow-on FLEX–2 experiments are exploiting the microgravity environment to study the spherically symmetric combustion of liquid droplets. · extracted · PSI investigation

220R001 · gravity: microgravity

Source

psi-data/PSI-69/Experimental table/PSI-69_Experimental table_FLEX.csv · row=37;column=O initial ambient composition; mole fraction · O initial ambient composition; mole fraction · extracted · PSI investigation

Source

psi-data/PSI-69/_investigation/PSI-69.json · section=objective · 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. · extracted · PSI investigation

Source

nasa/iss-combustion-guide-2015/np-2015-10-034-jsc_combustion_in_reduced_gravity-iss-mini-book-011116-508.pdf · page=36 · FLEX and the follow-on FLEX–2 experiments are exploiting the microgravity environment to study the spherically symmetric combustion of liquid droplets. · extracted · PSI investigation

220R002 · gravity: microgravity

Source

psi-data/PSI-69/Experimental table/PSI-69_Experimental table_FLEX.csv · row=38;column=O initial ambient composition; mole fraction · O initial ambient composition; mole fraction · extracted · PSI investigation

Source

psi-data/PSI-69/_investigation/PSI-69.json · section=objective · 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. · extracted · PSI investigation

Source

nasa/iss-combustion-guide-2015/np-2015-10-034-jsc_combustion_in_reduced_gravity-iss-mini-book-011116-508.pdf · page=36 · FLEX and the follow-on FLEX–2 experiments are exploiting the microgravity environment to study the spherically symmetric combustion of liquid droplets. · extracted · PSI investigation

224F001 · gravity: microgravity

Source

psi-data/PSI-69/Experimental table/PSI-69_Experimental table_FLEX.csv · row=39;column=O initial ambient composition; mole fraction · O initial ambient composition; mole fraction · extracted · PSI investigation

Source

psi-data/PSI-69/_investigation/PSI-69.json · section=objective · 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. · extracted · PSI investigation

Source

nasa/iss-combustion-guide-2015/np-2015-10-034-jsc_combustion_in_reduced_gravity-iss-mini-book-011116-508.pdf · page=36 · FLEX and the follow-on FLEX–2 experiments are exploiting the microgravity environment to study the spherically symmetric combustion of liquid droplets. · extracted · PSI investigation

solid

PSI-26: 22.7% · 1 source records

Show test IDs and sources

54 · gravity: microgravity

Source

psi-data/PSI-26/Science Documents/PSI-26_Science Documents_As Run_Test Matrix.xlsx · sheet=as run matrix;row=55;column=O2 % by volume · O2 % by volume · extracted · PSI investigation

Source

psi-data/PSI-26/_investigation/PSI-26.json · section=title · Burning and Suppression of Solids · extracted · PSI investigation

Source

psi-data/PSI-26/Science Documents/PSI-26_Science Documents_FlammabilityAspectsofFabric_USNationalCombustion.2013.docx · paragraph=17 · Microgravity combustion tests burning fabric samples were performed aboard the International Space Station. · extracted · PSI investigation

Excluded ambient records: 1.

PSI-25 · F4 · 0.174 1

Source

psi-data/PSI-25/Experimental table/PSI-25_Experimental table_BASS-II.csv · row=26;column=Calibrated initial O2 % by vol · Calibrated initial O2 % by vol · extracted · PSI investigation

Burner oxygen

Oxygen flowing from the burner, not the cabin:

PSI-159: 85.0% · 79 source records

Show test IDs and sources

21202 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=17;column=XO2 · XO2 · extracted · PSI investigation

21202 A2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=18;column=XO2 · XO2 · extracted · PSI investigation

21202 A3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=19;column=XO2 · XO2 · extracted · PSI investigation

21202 A4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=20;column=XO2 · XO2 · extracted · PSI investigation

21202 H1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=21;column=XO2 · XO2 · extracted · PSI investigation

21202 H2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=22;column=XO2 · XO2 · extracted · PSI investigation

21202 H3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=23;column=XO2 · XO2 · extracted · PSI investigation

21202 H4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=24;column=XO2 · XO2 · extracted · PSI investigation

21202 J1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=25;column=XO2 · XO2 · extracted · PSI investigation

21202 K1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=26;column=XO2 · XO2 · extracted · PSI investigation

21202 K2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=27;column=XO2 · XO2 · extracted · PSI investigation

21202 L1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=28;column=XO2 · XO2 · extracted · PSI investigation

21209 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=29;column=XO2 · XO2 · extracted · PSI investigation

21209 A2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=30;column=XO2 · XO2 · extracted · PSI investigation

21209 A3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=31;column=XO2 · XO2 · extracted · PSI investigation

21209 A4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=33;column=XO2 · XO2 · extracted · PSI investigation

21209 B1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=32;column=XO2 · XO2 · extracted · PSI investigation

21209 B2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=39;column=XO2 · XO2 · extracted · PSI investigation

21216 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=41;column=XO2 · XO2 · extracted · PSI investigation

21216 A2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=42;column=XO2 · XO2 · extracted · PSI investigation

21216 A3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=43;column=XO2 · XO2 · extracted · PSI investigation

21216 A4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=44;column=XO2 · XO2 · extracted · PSI investigation

21216 A5

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=45;column=XO2 · XO2 · extracted · PSI investigation

21216 A6

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=46;column=XO2 · XO2 · extracted · PSI investigation

21216 B1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=47;column=XO2 · XO2 · extracted · PSI investigation

21216 H1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=50;column=XO2 · XO2 · extracted · PSI investigation

21216 H2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=51;column=XO2 · XO2 · extracted · PSI investigation

21222 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=54;column=XO2 · XO2 · extracted · PSI investigation

21222 A2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=55;column=XO2 · XO2 · extracted · PSI investigation

21222 A3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=56;column=XO2 · XO2 · extracted · PSI investigation

21222 A4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=57;column=XO2 · XO2 · extracted · PSI investigation

21222 A5

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=58;column=XO2 · XO2 · extracted · PSI investigation

21222 B1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=59;column=XO2 · XO2 · extracted · PSI investigation

21228 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=64;column=XO2 · XO2 · extracted · PSI investigation

21228 A2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=65;column=XO2 · XO2 · extracted · PSI investigation

21228 A3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=66;column=XO2 · XO2 · extracted · PSI investigation

21228 A4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=67;column=XO2 · XO2 · extracted · PSI investigation

21228 B1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=68;column=XO2 · XO2 · extracted · PSI investigation

21228 H1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=74;column=XO2 · XO2 · extracted · PSI investigation

21228 H2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=75;column=XO2 · XO2 · extracted · PSI investigation

21228 J1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=76;column=XO2 · XO2 · extracted · PSI investigation

21235 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=81;column=XO2 · XO2 · extracted · PSI investigation

21235 A2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=82;column=XO2 · XO2 · extracted · PSI investigation

21235 B1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=88;column=XO2 · XO2 · extracted · PSI investigation

21235 K1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=89;column=XO2 · XO2 · extracted · PSI investigation

21235 L1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=90;column=XO2 · XO2 · extracted · PSI investigation

21242 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=91;column=XO2 · XO2 · extracted · PSI investigation

21256 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=97;column=XO2 · XO2 · extracted · PSI investigation

21256 A2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=98;column=XO2 · XO2 · extracted · PSI investigation

21256 A3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=99;column=XO2 · XO2 · extracted · PSI investigation

21256 A4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=100;column=XO2 · XO2 · extracted · PSI investigation

21256 A5

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=101;column=XO2 · XO2 · extracted · PSI investigation

21256 B1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=104;column=XO2 · XO2 · extracted · PSI investigation

21256 H1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=106;column=XO2 · XO2 · extracted · PSI investigation

21256 H2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=107;column=XO2 · XO2 · extracted · PSI investigation

21256 H3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=108;column=XO2 · XO2 · extracted · PSI investigation

21256 H4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=109;column=XO2 · XO2 · extracted · PSI investigation

21256 H5

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=110;column=XO2 · XO2 · extracted · PSI investigation

21256 J1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=113;column=XO2 · XO2 · extracted · PSI investigation

21265 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=114;column=XO2 · XO2 · extracted · PSI investigation

21265 A2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=115;column=XO2 · XO2 · extracted · PSI investigation

21265 A3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=116;column=XO2 · XO2 · extracted · PSI investigation

21265 A4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=117;column=XO2 · XO2 · extracted · PSI investigation

21265 A5

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=118;column=XO2 · XO2 · extracted · PSI investigation

21270 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=131;column=XO2 · XO2 · extracted · PSI investigation

21270 A2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=132;column=XO2 · XO2 · extracted · PSI investigation

21270 A3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=133;column=XO2 · XO2 · extracted · PSI investigation

21270 A4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=134;column=XO2 · XO2 · extracted · PSI investigation

21270 H1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=136;column=XO2 · XO2 · extracted · PSI investigation

21270 H2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=137;column=XO2 · XO2 · extracted · PSI investigation

21270 H3

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=138;column=XO2 · XO2 · extracted · PSI investigation

21270 H4

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=139;column=XO2 · XO2 · extracted · PSI investigation

21270 H5

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=140;column=XO2 · XO2 · extracted · PSI investigation

21277 A1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=141;column=XO2 · XO2 · extracted · PSI investigation

21277 C1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=147;column=XO2 · XO2 · extracted · PSI investigation

21277 C2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=148;column=XO2 · XO2 · extracted · PSI investigation

21277 F1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=150;column=XO2 · XO2 · extracted · PSI investigation

21277 F2

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=151;column=XO2 · XO2 · extracted · PSI investigation

21277 M1

Source

psi-data/PSI-159/Experimental table/PSI-159_Experimental table_CFI-G_Inverse Flames.csv · row=152;column=XO2 · XO2 · extracted · PSI investigation

NASA challenge: “The intermediate oxygen concentration used on the Moon will likely be 30% or greater, with a corresponding pressure of 10.2 psi or less.” “To enable flexibility, spacesuits are filled with 100% oxygen to only 4.3 psi (pounds per square inch), where the Earth's pressure at sea level is 14.7 psi.” NASA challenge statement

Moon reference ≥30%; suit reference 100% at 4.3 psi.

µg vs 1 g, same sample, as recorded

The local SAFFIRE-II CSV header reads “?-g” in the source file; its original microgravity symbol is not preserved there. Values are shown as written. The thickness “037 mm” is flagged as ambiguous in the extraction.

Sample	?-g burn length	?-g spread length	1-g burn length	1-g spread rate	Thickness as recorded

Material family × investigation

Families and geometry are PYRION substring conventions; ambiguous names remain under other. Source strings are preserved below.

Family	Investigation	O₂	Flow	Gravity	Recorded strings
DBP	PSI-102	Not in extracted test rows	Not in extracted test rows	Not in extracted test rows	Raw descriptions Dibutyl Phthalate [not specified]
Kapton	PSI-101	Not in extracted test rows	0 cm/s – 8.1 cm/s	Not in extracted test rows	Raw descriptions Kapton [not specified]
Kapton	PSI-102	Not in extracted test rows	Not in extracted test rows	microgravity	Raw descriptions Kapton [not specified]
lampwick	PSI-101	Not in extracted test rows	0 cm/s – 8.1 cm/s	Not in extracted test rows	Raw descriptions Lampwick [not specified]
lampwick	PSI-102	Not in extracted test rows	Not in extracted test rows	microgravity	Raw descriptions Lampwick [not specified]
Nomex	PSI-25	21.0% – 22.2%	Not in extracted test rows	Not in extracted test rows	Raw descriptions Nomex natural (nomex III) [not specified]
Nomex	PSI-26	21.2% – 22.5%	Not in extracted test rows	Not in extracted test rows	Raw descriptions Nomex III Natural [not specified] Nomex blend 2 cm [not specified] nomex natural III [not specified]
Nomex	PSI-99	22.1%	20 cm/s	Not in extracted test rows	Raw descriptions PMMA & Nomex [not specified]
other	PSI-25	13.6% – 22.2%	Not in extracted test rows	Not in extracted test rows	Raw descriptions 0.5" black rod [rod] 1/2" clear rod [rod] 1/4 blac rod [rod] 1/4 black rod [rod] 1/4 clear rod [rod] 1/4" black rod [rod] 1/4" black rod [rod] 1/4" clear rod [rod] 100 micron film 2 cm wide [sheet] 2 cm 0.4 mm thick film [sheet] 200 micron 2 cm wide [not specified] 3/8" black rod [rod] 3/8" clear rod [rod] 3/8"clear rod [rod] 300 micron film 2 cm wide [sheet] 4 cm spherical section [sphere] 400 micron film 2 cm wide [sheet]
other	PSI-26	16.7% – 22.4%	Not in extracted test rows	Not in extracted test rows	Raw descriptions 1 cm sphere [sphere] 1 cm sphere wake [sphere] 1 cm wake sphere [sphere] 2 cm sphere [sphere] 2 cm sphere wake ign [sphere] candle [candle]
PMMA	PSI-25	14.2% – 22.2%	Not in extracted test rows	Not in extracted test rows	Raw descriptions 1 cm 0.2 mm PMMA film [sheet] 1 cm wide 200 micron thick PMMA [not specified] 1 cm wide PMMA 1 mm thick [not specified] 1 cm wide PMMA 2 mm thick [not specified] 1 cm wide PMMA 3 mm thick [not specified] 1 cm wide PMMA 5 mm thick [not specified] 1 mm thick PMMA 1 sided 2 cm [not specified] 1 mm thick PMMA 2 cm wide [not specified] 1/2" clear PMMA rod [rod] 100 micron PMMA film 2 cm wide [sheet] 2 cm 0.1 mm PMMA film [sheet] 2 cm 0.2 mm PMMA film [sheet] 2 cm 4 mm 1 sided PMMA slab [sheet] 2 cm 0.1 mm PMMA film [sheet] 2 cm 100 micron thick PMMA [not specified] 2 cm wide 5 mm thick 1 sided PMMA [not specified] 2 cm wide PMMA 2 mm thick [not specified] 2 cm wide PMMA 3 mm thick [not specified] 2 mm thick PMMA 2 cm wide [not specified] 200 micron PMMA film 2 cm wide [sheet] 2mm thick PMMA 1 sided 2 cm wide [not specified] 3 mm thick PMMA 2 sided 2 cm thick [not specified] 3 mm thick PMMA 1 sided 2 cm wide [not specified] 300 micron PMMA film 2 cm wide [sheet] 4 mm thick 1 cm wide PMMA slab [sheet] 4 mm thick 2 cm 2ide PMMA slab [sheet] 4 mm thick PMMA 2 cm wide [not specified] 5 mm thick PMMA 2 cm wide [not specified]
PMMA	PSI-26	15.9% – 22.6%	Not in extracted test rows	Not in extracted test rows	Raw descriptions 2 cm pmma sphere [sphere] PMMA 1 cm [not specified] PMMA 2 cm [not specified] PMMA slab [sheet] PMMA sphere 1 cm [sphere] PMMA sphere 2 cm [sphere] pmma 1 cm [not specified] pmma 2 cm [not specified] pmma slab [sheet] pmma slab oppsed [sheet] pmma slab opposed [sheet] pmma sphere [sphere]
PMMA	PSI-99	0.22..0.221, 0.221	20 cm/s	Not in extracted test rows	Raw descriptions PMMA [not specified] PMMA & Nomex [not specified]
Pyrell	PSI-101	Not in extracted test rows	0 cm/s – 8.1 cm/s	Not in extracted test rows	Raw descriptions Pyrell [not specified]
SIBAL	PSI-100	0.21..0.212	30 cm/s	Not in extracted test rows	Raw descriptions SIBAL Fabric [fabric]
SIBAL	PSI-25	16.4% – 20.8%	Not in extracted test rows	Not in extracted test rows	Raw descriptions 1 cm SIBAL [not specified] 1 cm SIBAL top side ign [not specified] 2 cm SIBAL [not specified] 2 cm Sibal moved igniter [not specified]
SIBAL	PSI-26	21.5% – 22.7%	Not in extracted test rows	microgravity	Raw descriptions SIBAL 1 cm [not specified] SIBAL 2 cm [not specified] SIBAL 2 cm opposed flow [not specified]
SIBAL	PSI-98	0.215..0.217, 0.215	20 cm/s	Not in extracted test rows	Raw descriptions SIBAL Fabric [fabric]
SIBAL	PSI-99	22.1%	20 cm/s	Not in extracted test rows	Raw descriptions Cotton-Fiberglass (SIBAL) [not specified]
silicone	PSI-101	Not in extracted test rows	0 cm/s – 8.1 cm/s	Not in extracted test rows	Raw descriptions Silicone [not specified]
silicone	PSI-102	Not in extracted test rows	Not in extracted test rows	microgravity	Raw descriptions Silicone Rubber [not specified]
silicone	PSI-99	21.5% – 22.1%	20 cm/s	Not in extracted test rows	Raw descriptions Silicone [not specified]
Teflon	PSI-101	Not in extracted test rows	0 cm/s – 8.1 cm/s	Not in extracted test rows	Raw descriptions Teflon [not specified]
Teflon	PSI-102	Not in extracted test rows	Not in extracted test rows	microgravity	Raw descriptions Teflon [not specified]
Ultem	PSI-26	21.9% – 22.5%	Not in extracted test rows	Not in extracted test rows	Raw descriptions ultem sheet [sheet]
wax	PSI-25	17.4%	Not in extracted test rows	Not in extracted test rows	Raw descriptions Japan Wax candle [candle]
wax	PSI-26	15.9% – 21.9%	Not in extracted test rows	Not in extracted test rows	Raw descriptions Japan Wax Candle wake [candle] candle paraffin wake [candle] candle Japan wax [candle] flat wax slab [sheet] paraffin wax candle [candle] paraffin wax slab [sheet] parrafin wax candle [candle] parrafin wax slab [sheet]

Material index

Material