Unresolved atlas coverage · not a NASA experiment
PMMALunar gravity28.5 % O₂66.2 kPa20 cm/s airflowMissing together: never tested together
Affected mission questions
Closest completed NASA evidence
- Saffire VI sample VI-4
- Saffire V sample V-3
- Saffire V sample V-4
- LUCI PMMA rod (simulated lunar gravity)Simulated lunar gravity: a spinning rocket, about 2.5 minutes, with Coriolis force; oxygen fell during the burn
- Saffire V sample V-2
Relevant publication findings (5)
- “Both blowoff and quenching limits were obtained at several oxygen concentrations.” PMMA rods in concurrent flow, abstract
- “These are the first-ever, extended-duration (greater than 25 seconds) combustion tests performed in simulated Lunar gravity.” Lunar Combustion Investigation, abstract
- “Previous testing at microgravity and Lunar gravity indicated that some materials burned to lower oxygen concentrations in low gravity than in normal gravity, although the low g extinction limit criteria are not the same as 1g due to time constraints in drop testing.” Microgravity vs Martian gravity, abstract
- “Quenching was observed when the flow became sufficiently weak that the flame could no longer provide adequate heat flux to compensate for the heat losses (conduction into the rod and radiation).” PMMA rods in concurrent flow, abstract
- “However, the ambient concentrations of carbon monoxide and carbon dioxide rose significantly with the PMMA tests exceeding the 1-hour carbon dioxide limit and the 24-hour carbon monoxide limit.” Saffire VI results, PDF p. 6
Planned NASA overlap
FM²: planned, no results counted. Overlaps gravity + material.
Published plan overlaps these dimensions only. Flow, sample geometry and full joint conditions are not matched here; no completed FM² results are counted.
FM² atmospheres and samples, abstractFM² atmospheres and samples, abstractFM² mission plan, abstract
Matched-condition research question
PMMA, 28.5 % O₂, 66.2 kPa, 20 cm/s airflow, lunar gravity. The closest record, Saffire VI sample VI-4, differs in gravity, pressure.
Gap and platform limitations
- MicroFire research-planning heuristic, not NASA prioritization or an endorsed experiment recommendation.
- Matched on the dimensions represented by this planner: material, gravity, oxygen, pressure and airflow only.
- Geometry, scale, duration, ignition, confinement, orientation, hardware and sample history remain unmodelled.
- Coverage only: no prediction of outcome, information entropy, feasibility, cost, crew risk, TRL, schedule, funding priority or safety impact.
- Curated questions are not a survey of demand; repeated wording or extra scenarios can bias breadth.
- LUCI provides simulated lunar gravity, not Moon-surface measurements. Current atlas coverage is not the complete NASA archive.
- Analogous support counts rows matching the requested material with at most two mismatched condition dimensions; it is not evidential strength. Closest links may include more distant rows. Families describe the five closest records and five selected findings.
- Simulated lunar gravity: a spinning rocket, about 2.5 minutes, with Coriolis force; oxygen fell during the burn

