INSIGHTS / PURE CLIENT

Oxygen, hardware, and the data gap

A structural view of the curated catalog: where oxygen conditions sit, which hardware family produced what, and what NASA has not measured yet.

Oxygen concentration across the catalog

Each marker is the highest documented test O2 concentration for that investigation. Reference lines mark Earth air, the likely lunar-base floor, and the CFI-G maximum.

21% to 85% documented
Catalog coverage

Counts overlap: one investigation can serve several pillars, fuels or environments.

BY PILLAR

Prevention
11
Detection
4
Suppression
4

BY FUEL PHASE

Solid
5
Liquid
3
Gaseous
4
No fuel
4

BY TARGET ENVIRONMENT

Spacecraft cabin
16
Space station
15
Lunar base
7
Mars base
7
Pressurized rover
4
Spacesuit
3

HARDWARE MAP

Three families, plus the free-flyers

Filter the catalog
Combustion Integrated Rack (CIR)
ACME group

Modular ACME hardware for laminar gaseous non-premixed flames. Six sub-experiments share one chamber insert, burner set and imaging suite.

Six ACME sub-experiments: BRE / CLD Flame / E-FIELD Flames / Flame Design / s-Flame / CFI-G. BRE emulates condensed-fuel burning with a flat porous gas burner.

2 catalog records

Combustion Integrated Rack (CIR)
MDCA group

Multi-user Droplet Combustion Apparatus for liquid fuel droplets. FLEX, FLEX-2 and CFI use the same droplet deployment, ignition and imaging capability.

Microgravity Science Glovebox (MSG)
SPICE duct group

The modular fan-driven flow duct built for SPICE. BASS, BASS-II, SPICE and SLICE all use the same MSG duct hardware.

Built only from the curated catalog and public NASA/PSI summaries. No partial-gravity combustion data exists in PSI yet; LUCI and FM2 are the expected additions. Rocket and propellant fire safety is out of scope.