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#1301 |
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India under construction.
Join Date: Jun 2007
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anyone knows how many cryogenic engines we have left? i think russia gave us 4 of them and we used most of the engines.
what is the status on our indigenous engine?
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kabacreations |
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#1302 |
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nosce te ipsum
Join Date: Feb 2010
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#1303 |
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No frills attached.
Join Date: Aug 2006
Location: Pittsburgh
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GSLV is using cryogenic engines. We have a launch scheduled in the coming months, you can find it mentioned on the previous page. So far our indigenous cryogenic engines haven't succeeded, so this launch will be a test of that, fingers crossed !!!!!!!!!
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Cuts like a knife , .. but it feels so right baby!!!!!!!!!! Please visit my photo collection: Boston, New York, Pittsburgh and many more destinations to follow !!! Mihir1310's Photography |
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#1304 |
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Join Date: Jan 2011
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ISRO will test with GSLV without a cyro stage.
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Byakti 1 : Bangali Jago ! Byakti 2 : Ah ! Bangalir Kancha Ghum Bhangio Na ! |
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#1305 |
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nosce te ipsum
Join Date: Feb 2010
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Cryo stage for GSLV 3 is planned for Mid 2012 and April 2013.
From the annual report ![]() ![]()
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#1306 |
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Join Date: Aug 2010
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I need some technical help
Comparing the rocket Ariane 5 (EU) to GLSV III (a) So India needs to probably get to GLSV IV to match Ariane 5? in terms of lifting capacity? (b) Payload to LEO? Whats that (c) Payload to GTO? Whats that. (d) Whats the central aim of GLSV III? Extra lifting capacity in LEO or extra in GTO?
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Last edited by MeMumbaikar; April 30th, 2012 at 05:45 PM. |
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#1307 | |
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nosce te ipsum
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#1308 |
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I see
Did not think of it from the cost POV. Thankyou for the response. Another question I had is, from a commercial POV if GSLV III is operational fully. Does that mean ISRO can offer a lot of services offered by Ariane 5 at a much cheaper rate? Who are the potential customers who ISRO is trying to get on board? I read its specifically for the INSAT-4 series satellites of India which till now had been launched by Ariane 5. One final question. I notice that Insat-4 series offers Ku band frequencies which are needed for satellite broadcasting as well as C band ones. Isnt the launch of Ku bands not good for India considering we have lots of rains for months on end which affects the Ku and C bands? So what i can take from your answers thinktank is that India needs to GLSV III in order to launch the INSAT-4 series of heavy satellites (currently launch by Ariance 5) which are needed by mostly satellite and ditigal television broadcasting in the microwave spectrum. In the future they will make the GLSV III cheaper than Ariane 5 so that other countries (who are they?) can use the GLSV as a cheap and affordable means.
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Last edited by MeMumbaikar; April 30th, 2012 at 08:21 PM. |
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#1309 | |
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nosce te ipsum
Join Date: Feb 2010
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Quote:
Liquid hydrogen: about $9/kg Liquid Oxygen: $4/kg Excluding the cost of the rocket. -------- btw, Ku band weather problem can be sorted out using ground filters. --------- Specs: Ariane 5, Delta IV and GSLV Last edited by think-tank; April 30th, 2012 at 08:49 PM. |
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#1310 |
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thankyou for the info think tank
i guess i understand ISRO better now, its not about technology it is about cost. |
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#1311 | |
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#1312 |
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BANNED
Join Date: Oct 2011
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^ I wonder how railways will be able to afford all this, wasn't the price hike stopped by hitler didi ?? or is this Another grand plan of making the railways banckrupt
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#1313 | |
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#1314 | |
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#1315 | |
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#1316 |
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nice plan from ISRO. Fingers crossed for all of them.
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#1317 |
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BANNED
Join Date: Oct 2011
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As far as I know, there are two separate launches planned for GSLV III in the next 6 months, one will be without cryogenic engine, and the other one will be with it..
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#1318 | ||
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Quote:
b) Low Earth Orbit: Typically the kind of orbit remote sensing satellites go to - it's at a lower height and satellites in such orbits go around the earth multiple times in 24 hrs. PSLV typically takes satellites to LEO. Payload to LEO is how much weight a launcher get get to LEO. c) Geostationary Transfer Orbit: Geostationary satellites (like INSAT) that go around the earth in 24 hrs, and hence always stay "fixed" above certain geography - they go to GTO. GSLV/Ariane typically take satellites to this orbit. Payload to GTO for a launcher would always be much smaller than payload to LEO, since it takes a lot more fuel/power to get to GTO. d) GSLV III would have extra lifting capacity for both for LEO and GTO. However, it will primarily used for GTO. PSLV can manage LEO quite well. Quote:
Top of the line communication satellites these days weigh over 5000 kg. Even medium lift GSLV Mk III would not have sufficient capacity to carry some of the heavier satellites. We'll have to inevitably go to GSLV IV. Specially if India is serious about manned space flight, higher lift capacity is a must. This is not to say that there's not a robust market for services of launchers like PSLV or current version of GSLV (once it becomes reliable), but continuous improvement in lift capacity would be required, while keeping an eye on costs. |
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#1319 | |
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But liquid propulsion is a must for longer burns to take payloads to longer distances. Liquid propulsion: 1) Provides more control in guiding the rocket 2) Is much more efficient from a thrust to weight ratio point of view Cost of propellant (even the more expensive liquid ones) is small compared to the total cost of the rocket/launch. What is more expensive is the R&D required to perfect the liquid propulsion technology, and manufacturing of engines and storage mechanism for fuel (specially for cryogenic fuel), as it is much more complex than solid. I'm sure ISRO would love to perfect the cryogenic engine technology. It's not by choice that they have not been successful so far. Once they are successful (which I'm sure they will be, soon), you'll see them using it a lot more. Even futurist vision of cheap space travel relies on airbreathing ramjet engines (the kind Kalam talked about a lot) that use liquid fuel. |
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#1320 | |
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nosce te ipsum
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