| タイトル | Fire Detection Tradeoffs as a Function of Vehicle Parameters |
| 本文（外部サイト） | http://hdl.handle.net/2060/20170000248 |
| 著者（英） | Meyer, Marit E.; Dietrich, Daniel L.; Ruff, Gary A.; Urban, David L.; Booker, John E. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2016-07-10 |
| 言語 | eng |
| 内容記述 | Fire survivability depends on the detection of and response to a fire before it has produced an unacceptable environment in the vehicle. This detection time is the result of interplay between the fire burning and growth rates; the vehicle size; the detection system design; the transport time to the detector (controlled by the level of mixing in the vehicle); and the rate at which the life support system filters the atmosphere, potentially removing the detected species or particles. Given the large differences in critical vehicle parameters (volume, mixing rate and filtration rate) the detection approach that works for a large vehicle (e.g. the ISS) may not be the best choice for a smaller crew capsule. This paper examines the impact of vehicle size and environmental control and life support system parameters on the detectability of fires in comparison to the hazard they present. A lumped element model was developed that considers smoke, heat, and toxic product release rates in comparison to mixing and filtration rates in the vehicle. Recent work has quantified the production rate of smoke and several hazardous species from overheated spacecraft polymers. These results are used as the input data set in the lumped element model in combination with the transport behavior of major toxic products released by overheating spacecraft materials to evaluate the necessary alarm thresholds to enable appropriate response to the fire hazard. |
| NASA分類 | Space Transportation and Safety |
| レポートNO | GRC-E-DAA-TN32263 |
| 権利 | No Copyright |
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