摘要: The formation of secondary smoke in a solid rocket plume and the attenuation of a laser signal through it have been modelled by codes DROP-4 and OSA-4. Condensation nuclei have been characterized and number and size distribution m... 展开
| 作者 | Miller, E. | ||
|---|---|---|---|
| 原报告号 | ADA1142595 | 总页数 | 5 |
| 主办者 | Non Paid ADAS | ||
| 报告分类号 | [81G - Rocket Engines & Motors81A - Combustion & Ignition81H - Rocket Propellants] | ||
| 报告类别/文献类型 | AD / NTIS科技报告 | ||
| 关键词 | Exhaust plumes Rocket exhaust Solid propellant rocket engines Radiation attenuation Laser beams Laser guidance Computerized simulation Smoke Thermodynamics Condensation nuclei Aerosols Light scattering Smokeless propellants Mathematical models DROP-4 computer program OSA-4 computer program Secondary smoke | ||
