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Radiative Heat Transfer in Solid Rocket Nozzles
- Source :
- Journal of Spacecraft and Rockets. 57:247-260
- Publication Year :
- 2020
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2020.
-
Abstract
- The radiative heat transfer within solid propellant rocket motor nozzles due to the emission and isotropic scattering by the liquid-phase alumina particles present in the combustion products is inv...
- Subjects :
- Propellant
020301 aerospace & aeronautics
Materials science
Nozzle
Aerospace Engineering
02 engineering and technology
Mechanics
Rocket motor
01 natural sciences
010305 fluids & plasmas
Quantitative Biology::Subcellular Processes
Physics::Fluid Dynamics
Boundary layer
0203 mechanical engineering
Space and Planetary Science
Thermal radiation
Isotropic scattering
Attenuation coefficient
Combustion products
0103 physical sciences
Solid-fuel rocket
Chemical equilibrium
Subjects
Details
- ISSN :
- 15336794 and 00224650
- Volume :
- 57
- Database :
- OpenAIRE
- Journal :
- Journal of Spacecraft and Rockets
- Accession number :
- edsair.doi.dedup.....88cb87f932300c663653949a162253a4
- Full Text :
- https://doi.org/10.2514/1.a34598