by Chris Peterson » Sun Jul 12, 2015 3:17 pm
Javachip wrote:Does anyone out there know the ISO equivalent speed or sensitivity of New Horizon's imaging sensor in visual light, and what exposure times are typical for the images we are seeing?
ISO specs are more about marketing than they are about anything else. The concept has little relevance for scientific cameras. For those, what matters is the quantum efficiency (the percentage of photons that are recorded), and the dynamic range (the number of photons that a pixel can hold, modified by the intrinsic noise floor).
LORRI uses a thinned, backside illuminated CCD, which means it has a QE approaching 100% at its peak wavelength response (about 700 nm). It's a panchromatic camera (350-850 nm response) that produces monochromatic images. It is designed for typical exposure times of 50-200 ms, which is very fast for an astronomical camera but required because of the rapid motion of the target during flyby. At 100 ms, the image drift on the sensor from the spacecraft pointing stability is on the order of one pixel. The sensor is 1K pixels square (so a 1 MP device). With its 2630 mm focal length, f/12.6 optics it has a resolution of 1 arcsecond per pixel.
The mission goal is to image Pluto with a S/N greater than 100 at flyby.
[quote="Javachip"]Does anyone out there know the ISO equivalent speed or sensitivity of New Horizon's imaging sensor in visual light, and what exposure times are typical for the images we are seeing?[/quote]
ISO specs are more about marketing than they are about anything else. The concept has little relevance for scientific cameras. For those, what matters is the quantum efficiency (the percentage of photons that are recorded), and the dynamic range (the number of photons that a pixel can hold, modified by the intrinsic noise floor).
LORRI uses a thinned, backside illuminated CCD, which means it has a QE approaching 100% at its peak wavelength response (about 700 nm). It's a panchromatic camera (350-850 nm response) that produces monochromatic images. It is designed for typical exposure times of 50-200 ms, which is very fast for an astronomical camera but required because of the rapid motion of the target during flyby. At 100 ms, the image drift on the sensor from the spacecraft pointing stability is on the order of one pixel. The sensor is 1K pixels square (so a 1 MP device). With its 2630 mm focal length, f/12.6 optics it has a resolution of 1 arcsecond per pixel.
The mission goal is to image Pluto with a S/N greater than 100 at flyby.