contd..
So these solar panels are then connected to rechargeable batteries placed inside the satellite, or the power is directly fed to the devices live. But this then limits the operability of the satellite as any satellite involving this technology cannot to afford to be shadowed by any celestial object or lose power if any shadowing happens! One more problem with connecting the solar panels directly to the devices is that, if the power required is too high, then the wet area of solar panel must also be large enough to be able to generate so much power, hence causing cost and manufacturing issues. The efficiency of solar panels (recent developments) is between 30-40%!!
Weight is not of a concern here. why? Any guesses?
Hence, logical solution is to connect the solar panels to a rechargeable battery and simply connect the devices to that battery. The most preferred battery type is Ni-Cd/Ni-H2(for non-chemistry guys -> nickel-cadmium or nickel-hydrogen) battery system. But slowly, Lithium-Ion batteries are catching up, given their weight and power/weight ratio advantages, slowly space field is opening up to adopt lithium ion batteries.
Some may be wondering the meaning behind the last sentence above, well whether you know it or not, space technology is very very conservative, and we do not believe in changing anything that has worked so far! Hence, although space engineering sounds like a hi-tech field, its actually very very low tech if seen in real technology parameters or tech-specs.
Thirdly, the RTG's (Radio-Isotope Thermal Generators): Nothing but mini-nuclear plants, use mostly Pu-238(Plutonium-238) for its safety and low decay rate. But the efficiency of such a system is around 8%. But naturally, the advantages provided by this independent power system is well known from the defence technology. Satellites using RTG's can remain longer in eclipse/shadows or fly deeper in our galaxy, say beyond jupiter (>5 AU). Moreover, such independent power sources, help in reducing overall costs by eliminating the need for solar panels. Mostly used in landers or missions designed for deep space(beyond earth's orbit into dark space away from the sun).
But an RTG' on board brings in following complications:
1. safety/Shielding the space craft from radiation
2. excess heat radiation
3. Very expensive!
4. environment unfriendly (if landing on other planets, might cause mutation, and we might end up having to fight star wars or to see some hulks invading earth.)
Source:
http://upload.wikimedia.org/wikipedi...n_GPHS-RTG.jpg
P.S: European Space Agency (ESA) has a policy not to use RTG's at all even for missions beyond jupiter!
It is very safe to use system and has been space proven several times over and over again.
Further, lets go into the details of the Power distribution system. Like what we have even in our electricity supply, power is generated at one point and served to various places through a grid system. The satellite too utilizes a similar system but this being smaller in size and more or less controlled by on-board computers. There will be mostly a dedicated computer called "Power Control and Distribution Unit-PCDU" available on board satellites (cheapers one's - hmmm! its like buying a lx model in satellite which lacks abs, and airbags). So this PCDU, monitors the power generated at the solar panel and makes sure that battery is charged and always remains fully charged or charges the battery to max. possible level whenever the energy levels drop and simultaneously the solar generator is producing power! This also ensures that the batteries are not either over-charged or over discharged. In order to protect over charging, several shunting and resistors are used and to prevent over-discharging, certain safety margins are pre-set while programming the PCDU. This triggers a system shut-down or pushes the satellite into a so-called safe-mode where only the very essential devices such as the ones required to keep the satellite in orbit are kept on and remaining ones are put to sleep.
Image of a PCDU box.
Source:
http://www.astrium.eads.net/media/im...wer-pcdu01.jpg
Finally, the device level usage will be quite clear to everyone. Isn't it? Its like, you have power at home, all we need to do is to turn the switch to on position and bingo, light glows! (well unless your bulbs have fused out and still you call your local EB office to file a complaint!! in such a case, please consult a doctor immediately.
)
So a power control logic looks like as below:
Can somebody, explain me the above image? Electrical/electronics guys..anybody?
If you believed me on that!! Just kidding!!! Wanted to wake you guys up after reading a boring post!
The actual overall setup looks something like this below:
https://directory.eoportal.org/image...=1339683956438
The overall(full satellite) architechture looks as below:
https://directory.eoportal.org/image...=1344353440706
And finally, an interesting image: Exploded view of a full satellite:
http://ars.els-cdn.com/content/image...000636-gr4.jpg questions??
Quote:
Originally Posted by CLIX Reminds me of the days my friends & I used to rush to the little library in the street corner to get the Pop Science magazines before anyone else - in those days our only source of interesting info.
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Quote:
Originally Posted by dhawcash
Also, What kind of surface areas do satellite solar panels have? their wattage?
What kind of batteries do they use (AFAIK batteries have limited life spans) ?(Regarding the dark periods when they are in the shadow of earth receiving no sunlight) I guess these are the lifeline of the satellites as it would be dead if any of these systems fail. |
Hope I have answered your doubts in the above posts! Feel free to ask if you need more info.