Different experiments.
Clearer decisions.
Compare conditions, methods and findings without losing the context.
Full name
Spacecraft Fire Safety Demonstration I
Objective
Measure heat release and compare to spacecraft temperature/pressure rise
Fuel
Solid · SIBAL Cloth / One-Sided PMMA / Two-Sided PMMA +6 more
O₂ tested
21–31%
Pressure
100.0 kPa / 54.1 kPa / 55.2 kPa +4 more
Airflow
20 cm/s / 30 cm/s / Uniform flow across samples drawn by fans +1 more
Sensors
thermocouple / carbon dioxide sensor / gas sensors / side view cameras +19 more
Hardware
Cygnus spacecraft
Top finding
For Saffire VI, the outlet gas sensor was moved to the verified location at the end of the duct to provide oxygen consumption calorimetry.
Evidence
6 papers · 19 findings
AI comparison.
A written comparison of the selected experiments, drawn from their indexed papers.
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Complementary evidence, not interchangeable tests.
Match the fuel and atmosphere to your question.
Values are rolled up from AI-extracted test conditions across each experiment's papers. “—” means nothing extracted yet. Check the source papers for run-level values.