- #1
drod31
- 1
- 0
Hello Everybody,
I'm having issues defining a set of equations that calculates the Temperature of a black body object when provided with one of the following:
The goals is to define a temperature profile of a rocket during its trajectory. If I assume the detector is far enough that the rocket can be considered a point source how can I find the temp profile when given intensities/radiance/etc. at each time step?
Also worth mentioning... at the moment I'm not accounting for atmospheric changes.
I can get the temperature pretty easy when the spectral irradiance is provided (based on online literature).
Any sources that provide examples would be great!
Thanks!
I'm having issues defining a set of equations that calculates the Temperature of a black body object when provided with one of the following:
- Radiant Intensity [W sr-1]
- Spectral Intensity [W sr-1 m-1]
- Radiance [W sr-1 m-2]
- Spectral Radiance [W sr-1 m-3]
- Irradiance Flux Density [W m-2]
- Spectral Irradiance [W / m-3]
The goals is to define a temperature profile of a rocket during its trajectory. If I assume the detector is far enough that the rocket can be considered a point source how can I find the temp profile when given intensities/radiance/etc. at each time step?
Also worth mentioning... at the moment I'm not accounting for atmospheric changes.
I can get the temperature pretty easy when the spectral irradiance is provided (based on online literature).
Any sources that provide examples would be great!
Thanks!