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Spacecraft Fire Safety
Fire Prevention and Material Flammability

Material flammability may be the most critical element of an effective fire prevention program. Tests to assess material flammability have been in place since the early days of manned spaceflight and today materials are screened for use in spacecraft using a suite of 18 tests defined in NASA-STD-6001: Flammability, Odor, Offgassing, and Compatibility Requirements and Test Procedures for Materials in Environments that Support Combustion (PDF; 350 KB).

The Primary Test

Flammability test
Material being tested for flammability according to procedures spelled out in NASA-STD-6001, Test 1.

The most important flammability screening test is Test 1, the “Upward Flame Propagation” test. It is conducted in a normal gravity environment, with ambient conditions (gas composition and pressure) equal to that of the worst-case environment to which the material could be exposed. As shown in the diagram on the right, a vertical strip of material (typically 5 cm wide, 33 cm long, and of the worst-case thickness) is ignited at the bottom and scientists measure how far the flame spreads up the strip. The material fails the test when more than 15 cm burns or flaming debris drips onto a piece of paper placed 20 cm below the sample.

Additional Tests

Test 1 was designed to represent a worst-case assessment of material flammability aboard spacecraft. However, research conducted in microgravity has shown that burning materials behave quite differently under the non-buoyant conditions of microgravity than under gravity-driven convection conditions. Materials that fail Test 1 may still be used on spacecraft but must undergo further testing and analysis according to NASA-STD-6001. One of the additional tests -- ”Heat and Visible Smoke Release Rates” -- uses a standard cone calorimeter (a special lab instrument that uses an oxygen-consumption technique to measure the rate of heat release of materials) to provide data on ignition delay times and burning rates of materials. However, this test is also affected by gravity-induced buoyancy, so the relationship between these data and the behavior of materials in microgravity is not known.

It is important for the FPDS program to develop material flammability tests that yield data from which the flammability of the material in microgravity can be determined. A second critical task for this program is to evaluate the flammability of materials in atmospheres that may be used in exploration spacecraft and habitats. Both of these tasks must take the gravity level (microgravity during transit between the Moon or Mars; 1/6 normal gravity on the Moon, and 3/8 normal gravity on Mars) into account in order to ensure that the best and safest possible material is used in spacecraft and space-based habitations.

Products

The major products of this effort are:

  • Normal gravity material flammability test to evaluate reduced gravity flammability
  • Material flammability assessment in candidate atmospheres for exploration transit vehicles and habitats

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FPDS Related Multimedia

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NASA-STD-6001 Test 1 diagram
A diagram of the NASA-STD-6001 Test 1 apparatus.

 

 

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FEANICS insert
Low-g material flammability tests will be conducted in the Flow Enclosure Accommodating Novel Investigations in Combustion of Solids (FEANICS) apparatus.

 

 

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Combustion Integrated Rack
The Combustion Integrated Rack (CIR) is a small laboratory for the International Space Station (ISS) that will accept experiment-specific inserts, such as FEANICS.
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Last Updated: June 1, 2005