A simple method for predicting rocket exhaust smoke visibility
Author:
Affiliation:
1. Naval Weapons Center, China Lake, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27981
Reference33 articles.
1. Theoretical Analysis of Turbulent Mixing of Reactive Gases With Application to Supersonic Combustion of Hydrogen
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1. Prediction of the Dissipation of a Solid-Rocket Contrail;Journal of Propulsion and Power;2000-09
2. Plume, Signal Interference and Plume Signature;Solid Rocket Propulsion Technology;1993
3. Prediction of the visible signature of solid rocket plumes;Journal of Spacecraft and Rockets;1990-01
4. Effects of multiple scattering on rocket exhaust plume smoke visibility;Journal of Spacecraft and Rockets;1989-07
5. Effect of Particle Size Distribution on the Radiosity of Solid-Propellant Rocket Motor Plumes;Spacecraft Radiative Transfer and Temperature Control;1982-01-01
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