Smoke and Aerosol Measurement Experiment (SAME) measures smoke properties, or particle size distribution, of typical particles from spacecraft fire smokes to provide data to support requirements for smoke detection in space and identify ways to improve smoke detectors on future spacecraft.Principal Investigator(s)
National Aeronautics and Space Administration (NASA)Sponsoring Organization
Human Exploration and Operations Mission Directorate (HEOMD)Research Benefits
Information PendingISS Expedition Duration:
April 2007 - September 2010Expeditions Assigned
15,23/24Previous ISS Missions
SAME is the successor to the Comparative Soot Diagnostics (CSD) experiment that flew aboard STS-75 in 1996. The experiment showed that smoke produced in low gravity is different from smoke produced in normal gravity (microgravity smoke particles are larger).
Spacecraft smoke detectors must detect different types of smoke. For example, hydrocarbon fuels typically produce soot and plastics produce droplets of recondensed polymer fragments. While paper and silicone rubber produce smoke comprised of liquid droplets of recondensed pyrolysis products. Each of these materials produces a different type of smoke, with particles of various sizes and properties.
Smoke and Aerosol Measurement Experiment (SAME) will assess the size and distribution of smoke particles produced by different types of material found on spacecraft such as, Teflon, Kapton, cellulose and silicone rubber. SAME will evaluate the performance of the ionization smoke detectors (used on Space Shuttles), evaluate the performance of the photoelectric smoke detectors (used on the ISS) and collect data for which a numerical formula can be developed and used to predict smoke droplet growth and to evaluate alternative smoke detection devices on future spacecraft.
The experimental design and practical application of the data will be complemented by the development of a numerical code to predict the smoke droplet growth as a function of the fuel pyrolysis rate, the thermodynamic properties of pyrolysis vapor, and the flow environment. SAME also has the capability to evaluate other fire detection/particulate sensing devices for the test materials. The results will provide statistics of the smoke particulate size distribution for a range of smoke generation conditions and measurement of a readily modeled reference for validation of smoke growth models.
The SAME experiment will provide technology for an advanced fire detector for future spacecraft that will be used for long duration missions. SAME will provide quantitative data on the sensitivity of these detectors to reduced gravity smokes that will allow evaluation of the adequacy of these existing technologies using relevant data. The current Fire Prevention, Detection, and Suppression (FPDS) program plan allows for the re-evaluation of future sensor technology, to allow new technology and capability to be utilized. The results from SAME are needed to provide the reduced gravity baseline data against which future detection technology developments can be evaluated.Earth Applications
The smoke detectors developed from the results of SAME can also be useful in other extreme environments on Earth, such as submarines or underwater laboratories. Accurate detection of smoke in these environments can save lives.
For SAME the crew will pyrolyze (decompose the material by extreme heat) basic spacecraft materials (Kapton, Silicon Rubber, Teflon and cellulose (lamp wick)) and a baseline material (Dibutyl Phthalates) in the MSG. There will be a total of twenty test points (each sample will be tested four times) . Each carousel (sample holder) can hold up to six samples. If time permits additional test points can be completed with the samples in the carousel.
After pyrolysis, the smoke is aged in a chamber to simulate the time it takes the smoke to build up and move to the detectors. Smoke, the product of the pyrolysis is characterized in the following ways:
SAME will use probes to heat a wire and drive the smoke onto a small collection grid (approximately 1/8 in. diameter) as it flows past using an effect know as thermophoresis (what causes dust to stick to the wall behind a radiator). At each test point, two samples of the smoke will be taken: the first within seconds of its generation and the second after a defined aging period, during which the size and shape of the smoke particulates will have changed. These sample grids will be returned to Earth from the ISS and examined under a transmission electron microscope.
The Smoke and Aerosol Measurement Experiment (SAME) was conducted in the Microgravity Science Glovebox (MSG) on the International Space Station (ISS) during Expedition 15. Overall, 30 samples were tested comprising of six samples each of five different materials: TeflonTM, KaptonTM, silicone rubber, cellulose, and dibutyl-phthalate (a chemical used to make flexible plastic) deposited on a porous wick. These were tested at different airflow rates, heating temperatures, and smoke aging durations.
Smoke properties from different materials were determined using detectors to measure different particulate sizes and their relative abundances in order to describe the overall smoke distribution. A substantial portion of the aerosol mass is in particles that are larger than 1 micron. Teflon smoke comprised primarily of particles having diameters less than 1 um. The effect of aging is consistent with particle coagulation with limited wall loss, the overall number count decreases substantially while the mass concentrations remain relatively steady. This is reasonable given the broader size distribution for silicone smoke containing significant numbers of both large and small particles. Although the arithmetic mean diameters are all in the 100 to 200 nanometer (nm) range, interpreting particle sizes by only one statistic can be deceptive due to the nature of the particle size distribution. In general, since the mass increases with the cube of the diameter, the larger particles do not affect the arithmetic mean diameter (AMD) as much as they affect the light scattering signal which corresponds with the particle mass. Consequently, although the AMD for silicone rubber is 227 nm, almost half the particle mass is larger than 1000 nm. The lamp wick showed similar behavior in the experiment.
All samples produced significant numbers of sub-micron particulate that are better detected using an ionization smoke detector, however a light scattering detector would perform very well for most of the cases. Depending on the conditions, results suggest broader smoke particulate size distributions can be produced from prefire overheat events, thus detection methods which can measure a wider spectrum of particulate size may show more successful and reliable detection. Spacecraft and associated missions outside of low Earth orbit will require increased reliability of fire detection systems in addition to robust false alarm resistance. Given the constrained space on any spacecraft, the target for the fire detection system is necessarily the early phase and not established flaming fires; consequently, the primary target for detection is the pre-fire heating products and not the soot and ash. This research will help to improve design of future detectors (Urban et al. 2009).
Urban DL, Ruff GA, Sheredy WA, Cleary T, Yang J, Mulholland G, Yuan Z. Properties of Smoke from Overheated Spacecraft Materials in Low-Gravity. 47th Aerospace Sciences Meeting and Exhibit, Orlando, FL; 2009 January 5-8
Urban DL, Ruff GA, Brooker JE, Cleary T, Yang J, Mulholland G, Yuan Z. Spacecraft Fire Detection: Smoke Properties and Transport in Low-Gravity. 46th Aerospace Sciences Meeting and Exhibit, Reno, NV; 2008
Urban DL, Ruff GA, Mulholland G, Cleary T, Yang J, Yuan Z. Measurement of Smoke Particle Size under Low-Gravity Conditions. SAE International Journal of Aerospace. 2009; 1(1): 317-324. DOI: 10.4271/2008-01-2089. [report number 2008-01-2089]
Ruff GA, Urban DL, King MK. A Research Plan for Fire Prevention, Detection, and Suppression in Crewed Exploration Systems. 43rd Aerospace Sciences Meeting and Exhibit, Reno, NV; 2005
Urban DL, Yuan Z, Ruff GA, Cleary T, Griffin D, Yang J, Mulholland G. Detection of Smoke from Microgravity Fires. SAE Technical Paper. 2005; 2005-01-2930. DOI: 10.4271/2005-01-2930.