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Post by sage on Aug 16, 2023 23:02:03 GMT
Right now, I'm trying to understand multi-frame blind deconvolution and phase diversity. When I am done, I will help yehang79 with the railgun problem and spacemancraig with finding the equation to Beam Quality.
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Post by yehang79 on Aug 17, 2023 11:43:05 GMT
I want to know if it is possible to obtain specific data of phased array radar, although it is very unlikely to get. By the way, thanks for your help!
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Post by sage on Sept 5, 2023 6:16:38 GMT
I want to know if it is possible to obtain specific data of phased array radar, although it is very unlikely to get. By the way, thanks for your help! Are you looking for data on Passive phased array radar or the new Active electronically scanned arrays, that have replaced them? Here is a link to a Air Power Australia Analyses of the Tikhomirov NIIP L-Band Active Electronically Steered Arraylook down towards the bottom for the graphs with the data
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Post by sage on Sept 24, 2023 19:17:04 GMT
After months and months of work I have finally found the answer for the time need to look for enemy space craft. After looking into the 300 rule, the 500 rule and the npf rule, I finally found the answer. It all has to do with angular speed and Field of View. Your angular speed will limit how long an object is in your field of view. Let's use the field of view of the Advanced Camera for surveys and the Wide Field Camera 3 for the Hubble space telescope to get the field of view examples. Advanced Camera for surveys Channel | Spectral Range (Nanometers) | Detector Array size (pixels) | Pixel Size (Microns) | Field of View (ArcSec) | Wide Field | 350-1050 | 4096 X 4096 | 15 X 15 | 200 X 204 | High Resolution | 200-1050 | 1024 X 1024 | 21 X 21 | 26 X 29 | Solar Blind | 115-180 | 1024 X 1024 | 25 X 25 | 26 X 29 |
Wide Field Camera 3 Channel
| Spectral Range
(Nanometers)
| Detector Array
size (pixels)
| Pixel Size
(arcsec)
| Field of View
(ArcSec)
| UVIS | 200-1000 | 4096 X 4096 | 0.04 | 160 X160 | NIR | 800-1700 | 1024 X 1024 | 0.13 | 123 X 137 |
Now let's list some angular speeds. Name of object | location | Angular speed (Arc Seconds per second) | James Webb Space Telescope | Lagrange point 2. Sun-Earth | 0.041 | International Space Station | 379 km from earth | 4060 | standing on earth | on the ground on earth | 15 |
Angular speed = 206265 X (speed of space craft/ altitude)
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Post by sage on Oct 7, 2023 22:09:22 GMT
Ok, I must be doing something wrong. I just plugged in some numbers, and it said that we would be able to see a 100 MW waste heat starship, from earth with a human I in a distance of light years from us. We know this is wrong. I will recheck my units and numbers to find the error. But if there is no error, then we can't use this equation to find space crafts.
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Post by sage on Oct 16, 2023 2:25:57 GMT
I found the problem. It that we are using the Boltzmann constant
What we need to do is use the Stefan-Boltzmann constant.
I don't know how I didn't see that before. It was till I check the units for IR tracking range that I found the problem.
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Post by sage on Oct 22, 2023 5:12:38 GMT
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Post by sage on Nov 6, 2023 1:11:59 GMT
Ok I may have to do a new posted with the update equations and info at this point. Also, I'm looking into our sensor range for laser and missiles.
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Post by sage on Nov 12, 2023 2:30:38 GMT
Right now, I'm adding some things missing from those equations and hope to fix them next week. When I have time off.
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Post by sage on Nov 21, 2023 3:24:33 GMT
Ok, I was just crossing all my T and doting all my eyes, when I was double checking my understanding of the Detector Bandwidth Factor.
And during which I noted a 0 region from 0-1000 um-K.
Here is a quote about the Detector Bandwidth Factor
Was any else able to find the same Universal black-body curve?
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Post by sage on Dec 3, 2023 21:39:36 GMT
Here the problem, if the temp times the wavelength falls into 0-1000 um-K (um is a 1000nm), it would produce stealth ships. Here is a table that I have been working on. Temp | wavelength | wavelength | k | um | nm | 293 | 3.413 | 3413 | 500 | 2 | 2000 | 1000 | 1 | 1000 | 1500 | 0.667 | 667 | 2000 | 0.5 | 500 | 2500 | 0.4 | 400 | 3000 | 0.333 | 333 |
Any sensors that bandwidth does not reach those values would make enemy spaceships invisible to your sensor. So, if the bandwidth of your sensors is .4um to 1um or 400nm to 1000nm, then you would be unable to see an enemy spaceship with radiator running below 1000k. It should be noted that 293 is the temp of our crew modules on our space craft. I'm looking more into sensor limitations right now and will get back to you. Do you guy think I should make a new post with my updated equations?
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Post by sage on Dec 9, 2023 3:19:30 GMT
Ok I have also worked on a table about where the peak energy would be as a function of wavelength for a set of temp(k). Temp | Peak Wavelength | Peak Frequency | k | nm | Thz | 293 | 9890 | 17.225 | 500 | 5796 | 29.393 | 1000 | 2898 | 58.79 | 1500 | 1932 | 88.18 | 2000 | 1449 | 117.59 | 2500 | 1159 | 146.97 | 3000 | 966 | 176.37 |
Also, I found a graph that shows them limited Black-body spectrum range per temp
As you can see 300(k), which is around 293(k) of our crew modules is just short of 1.5um in transmitting power that we could sense. While, 1000(k) is well with in the 1um to .4um range I was using as an example. Now I have to check to see how cold I can make our reactor without them breaking.
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Post by sage on Jan 7, 2024 1:20:58 GMT
Almost there, I will have to start a new post so it more clean, then what we have here. But I found a way around the problem that I had earlier, by using a LiTaO3 Pyroelectric Detector as a replacement for my Si/Pin Balanced Amplified Photodetectors.
The range of the LiTaO3 Pyroelectric Detector is 0.6 - 16 µm While the Si/Pin Balanced Amplified Photodetectors is 0.32 - 1 µm
The Noise Equivalent Power is
LiTaO3 Pyroelectric Detector 3248 nW Si/Pin Balanced Amplified Photodetectors 130nW
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Post by yehang79 on Jan 12, 2024 8:13:40 GMT
Nice work. I strongly appreciate it.
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Post by sage on Jan 14, 2024 5:53:46 GMT
Right now, I am seeing if I should use a LiTaO3 Pyroelectric Detector, or a combination of Photodiodes.
I also found out how to do the bandwidth factor for each sensor. The only problem is that I have to redo the bandwidth factor for change in temperature. I right now working on building tables for the NEP in Watts for each sensor and produce bandwidth factors for each temp per sensor.
Right now I'm going with the following temperatures. 293 K the temperature of crew modules, 500 K, 1000K, 1500 K, 2000K, 2500K and 3000K as they the listed temperature of our Radiators when we build them in the builder.
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