DTIC ADA114259: Smoke Dynamics of Solid Rocket pdf

DTIC ADA114259: Smoke Dynamics of Solid Rocket_bookcover

DTIC ADA114259: Smoke Dynamics of Solid Rocket

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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 measured from data obtained in the U.S. Army Missile Command’s Smoke Characterization Facility. Predictions from DROP-4 and OSA-4 compare satisfactorily with experimental flight data. (Author

  • Creator/s: Defense Technical Information Center
  • Date: 4/22/1982
  • Year: 1982
  • Book Topics/Themes: DTIC Archive, Miller, Eugene, MACKAY SCHOOL OF MINES RENO NV DEPT OF CHEMICAL AND METALLURGICAL ENGINEERING, *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

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