JSCh
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Yes. Also less than 48 hrs from the last launch from Jiuquan launch center.Is it the 3rd launch in 10 days?
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Yes. Also less than 48 hrs from the last launch from Jiuquan launch center.Is it the 3rd launch in 10 days?
ISRO own website says 8t LEO, you know more than them? Ok your gslv-3 is much better than ours, your space program is miles ahead, all right? satisfied ?
Bullshit, u Indians only good at boasting things on PowerPoint. Let's compare GTO then, ours 14t, your non existent gslv3 4t, got it?It is 8 tons to 620km high circular LEO while long march five is 25 tons to 200 km by 400 km eplitical LEO. They are not the same it takes more delta v to place at 620km than it does at 200-400 km. If long march 5 launched into 620km high orbit its capablity would be somewhere between 10 - 15 tons.
Besides MK-3 is in its base config which should have been flown back in 2012 but was delayed due to problems with ISRO's MK-2 rocket. Once the weakass engines in the core are replaced the rocket can do 6.5 ton GTO and around 15 ton LEO so not that much behind long march 5
Bullshit, u Indians only good at boasting things on PowerPoint. Let's compare GTO then, ours 14t, your non existent gslv3 4t, got it?
Bullshit, missing the critical cryogenic engine Indians boasting for years, which China flied 32 years ago on long march 3 in 1984GSLV MK-3 non-existent? Are you aware that it has already flown in suborbital config?
Really ?It is 8 tons to 620km high circular LEO
Bullshit, missing the critical cryogenic engine Indians boasting for years, which China flied 32 years ago on long march 3 in 1984
Really ?
Can you enlighten us with a source of this claim?
It is 8 tons to 620km high circular LEO while long march five is 25 tons to 200 km by 400 km eplitical LEO. They are not the same it takes more delta v to place at 620km than it does at 200-400 km. If long march 5 launched into 620km high orbit its capablity would be somewhere between 10 - 15 tons.
Besides MK-3 is in its base config which should have been flown back in 2012 but was delayed due to problems with ISRO's MK-2 rocket. Once the weakass engines in the core are replaced the rocket can do 6.5 ton GTO and around 15 ton LEO so not that much behind long march 5
If you go to ISRO website, they have a sub-GTO orbit too. What is a sub-GTO orbit?Is there such thing called high circular 620km LEO? Space lifting capacity is place according to 2 catergory LEO, GTO. I never heard high circular LEO. you don't make up another type and confuse us.
Funny how the advanced Indian staged combustion (cough* Russsian cyro copy) is not use in GSLV mk iii? But instead a gas generator CE-20 had to be used ...LOLYour YF-73 engine that flew in 84 was a gas generator design. Such design is childs play compared to stage combustion cycle that ISRO's CE-7.5 uses.
YF-73 specific impulse: 420 seconds
CE-7.5 specific impulse: 452 seconds
Look at wikipedia or ISRO's site