Combustion diagnosis for analysis of solid propellant rocket abort hazards: Role of spectroscopy
Solid rocket propellant plume temperatures have been measured using spectroscopic methods as part of an ongoing effort to specify the thermal-chemical-physical environment in and around a burning fragment of an exploded solid rocket at atmospheric pressures. Such specification is needed for launch s...
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| Veröffentlicht in: | Journal of physics. Conference series 2014-01, Vol.548 (1), p.12055-10 |
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| container_title | Journal of physics. Conference series |
| container_volume | 548 |
| creator | Gill, W Cruz-Cabrera, A A Donaldson, A B Lim, J Sivathanu, Y Bystrom, E Haug, A Sharp, L Surmick, D M |
| description | Solid rocket propellant plume temperatures have been measured using spectroscopic methods as part of an ongoing effort to specify the thermal-chemical-physical environment in and around a burning fragment of an exploded solid rocket at atmospheric pressures. Such specification is needed for launch safety studies where hazardous payloads become involved with large fragments of burning propellant. The propellant burns in an off-design condition producing a hot gas flame loaded with burning metal droplets. Each component of the flame (soot, droplets and gas) has a characteristic temperature, and it is only through the use of spectroscopy that their temperature can be independently identified. |
| doi_str_mv | 10.1088/1742-6596/548/1/012055 |
| format | Article |
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| subjects | Combustion Droplets Fragmentation Launches Payloads Physics Propellants Rocket propellants Rockets Solid propellants Solid rocket propellants Soot Spectroscopy Spectrum analysis |
| title | Combustion diagnosis for analysis of solid propellant rocket abort hazards: Role of spectroscopy |
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