
Now please launch the GSLV with Indian Cryo and GSLV MARK 3 - TD by year end ..... can't wait for those

I think the reference to Mauritus that is being mentioned is to the announcement " Mauritius confirms ..... " during launch.pentaiah wrote:congrats to all the ISRO personnel
one question Mauritius is west south west of Shrihari kota, and I guess the rocket is launched east wards why is that after launch Maritius is confirming the tracking should be east south east of India no?
Being far away from the mainland managing logistics could be an issue. Also space centers observe frequent visits of various delegations, domestic and foreign, and A&N being a major military base it could be uncomfortable to accommodate research and military at one place.Rahul M wrote:if we need a launch pad won't one in A&N island chains be a better option ?
Normally, when one stage burns out and the next stage ignites, there is a small coasting phase.SriKumar wrote: Unrelated observation: the rocket slowed down a bit during the 3rd stage when approaching 3rd stage separation.
Agreed. So what is intriguing is that this slowdown/coastaing phase exists only for the 3rd stage and not other stages. If you look at the velocity vs. time profile of the rocket at any time in the above video posted by pgbhat a few posts above; but let's pick timepoint 7:14 in the video, the only slowdown in the entire mission is during the 3rd stage. None of the earlier stages have a drop in the velocity profile. In addition, this 'coasting phase' lasts about 2 minutes. Watch the pgbhat video from 9:25 onwards...it shows the velocity profile again. PS3 separates around 9:41 and PS4 ignites around 9:52 (based on the vocal announcements which have a few seconds lag from the actual event). If we are to believe that PS3 shut down around 7:32 or later (per vocal announcement), PS3 is a dead weight and still going for the ride for a good 2 minutes before it separates. Very interesting.SSridhar wrote:Normally, when one stage burns out and the next stage ignites, there is a small coasting phase.SriKumar wrote: Unrelated observation: the rocket slowed down a bit during the 3rd stage when approaching 3rd stage separation.
That is exactly what I said.. change the grill and make it Mark II or III as you like it!There is an aesthetic quality to every vehicle launch
During coasting, they use the gravity to increase velocity without burning rocket fuel. In turn, the rocket loses ome altitude...In other words, some of the potential energy is converted into kinetic energy. This way it is supposed to be more efficient, as there is loss due to drag in outer space.So what is intriguing is that this slowdown/coastaing phase exists only for the 3rd stage and not other stages. I
I guarantee you the altitude never reduces for this rocket. Even in this 'coasting' phase, it is still going upward. Check range vs. altitude at 6:00 (or any other time point where they show the range vs. altitude). It never reduces. One could argue that range vs. altitude is not the same as time vs. altitude but I am confident for this rocket launch that range is always increasing monotonically with time. I dont know whether the reduction in velocity (which is only in the first decimal point or so: e.g. 5.5 km/sec to 5.4 km/sec or something like that) is a deliberate maneuver to make the separation easier by reducing some load, or do they need the time to 'prepare' the 4th stage for separation, or is it a 'holding mode' of sorts to adjust the velocity parameters for injection into orbit after the final stage ignites.geeth wrote:During coasting, they use the gravity to increase velocity without burning rocket fuel. In turn, the rocket loses ome altitude...In other words, some of the potential energy is converted into kinetic energy.So what is intriguing is that this slowdown/coastaing phase exists only for the 3rd stage and not other stages. I
it won't be farther away than guyana or similar proposals here ! or even sri lanka, the logistics problem would involve either a ship based transport or at a stretch -- air based one. neither is undoable.abhijitm wrote:Being far away from the mainland managing logistics could be an issue.Rahul M wrote:if we need a launch pad won't one in A&N island chains be a better option ?
errm, A&N is a fairly largish island chain and only a handful have any military presence (and those have a pretty high foreign tourist presence), the majority are uninhabited as well. this is not a problem.Also space centers observe frequent visits of various delegations, domestic and foreign, and A&N being a major military base it could be uncomfortable to accommodate research and military at one place.
A rocket at max can carry a payload which is close to its dead weight of its 4th stage. Otherwise satellite and rocket will tumble before separation. So if PSLV has to carry 3 tonnes, the empty last stage should have close to that weight. One option is to remove the 3rd stage and quadraple the engines for 4th stage (a costly option). Other one being, remove the current 3rd and 4th stage and add the cryo stage for GSLV Mk2dhiraj wrote:i think we also need to consider the orbit of the launches conducted by PSLV (so probably a 3 tonne launch for LEO is also possible for PSLV) ...the issue is ISRO started with conservative payloads during the initial flight for PSLV and never exploited its full potential....until recently with around 1800KG payload.....
My perception is that ISRO got really aggressive with its launch vehicle capability under G Madhavan Nair.....but the current ISRO again seems to look like the 80s-90s period ....very conservative....and taking there own sweet time......
The scientist who led the Vikas engine team and later headed the Cryo engine team is out of ISRO.....the boss who bought aggression in rocket launch capability is also out of ISRO...... No proper GTO capable rocket..... No heavy lift capacity.... get a sad feeling especially in competition with China.....
At least after today;s launch there could have been some announcement for Mark 3 and GSLV with Indian Cryo launch schedule and there status..... but NO News.....
Thanks. this explains the no slowdown from stage 1 to 2 (ullage) and stage 2 to 3 (retro). Am wondering why does it need 2 minutes to transition from stage 3 to 4. Stage 3 cuts off but does not separate for almost 2 minutes which seems like a very long time.symontk wrote:PSLV second stage has both ullage and retro rockets. So after PS1 cutoff, ullage rockets take the rocket forward before the PS2 ignition. After PS2 cutoff, retro rockets fire, and push back the PS2. However there are no ullage or retro rockets for PS3 or PS4. Thats why there is a coasting phase needed after PS3 cutoff
Since PS2 has ullage rockets, the velocity of the rocket is not impacted and so the liquid fuel of the PS2 will be closer to the engine below. However there are no ullage rockets for PS4 and so the sudden decelration will put pressure on the upper chamber of liquid fuel containers. I am not aware of the exact dynamics to the time, maybe it requires 2 minutes to stabilize and bring the fuel pressure normal. Also remember its almost vaccum at that heightSriKumar wrote:Thanks. this explains the no slowdown from stage 1 to 2 (ullage) and stage 2 to 3 (retro). Am wondering why does it need 2 minutes to transition from stage 3 to 4. Stage 3 cuts off but does not separate for almost 2 minutes which seems like a very long time.symontk wrote:PSLV second stage has both ullage and retro rockets. So after PS1 cutoff, ullage rockets take the rocket forward before the PS2 ignition. After PS2 cutoff, retro rockets fire, and push back the PS2. However there are no ullage or retro rockets for PS3 or PS4. Thats why there is a coasting phase needed after PS3 cutoff
There could be a secret technology restriction regime which we may not be aware.Singha wrote:our heavy launcher program has fallen into a rut for various reasons. next 2 yrs if we cannot proof the desi cryogenic engine on a couple of flights, things will get bad...there are no more rus cryogenic engines left anyway. we need to maintain a higher launch frequency also to improve comms , C3I , SAR , Sigint, IMINT ..... many of these even the PSLV can do, but our production and launch rate of PSLV again is quite low.
meantime Cheen is investing heavily in improving and adapting its successful long-march heavy launchers and looks on the verge of being able to attack Ariane on price front.
The (ex)British Guiana (the current "Guyana" contiguous to the other Guiana's) has a majority population of PIOsvina wrote: Ideally once we get the GSLV MKIII and IV versions in, we should get in touch with the Brazilians / Ariane and build a launch pad for these vehicles ,also PSLV in Brazil's Alicantra space center or in Korou. That will allow us to haul a couple of hundred kgs more to orbit as they are bang on the equator. The Russians for eg, have built a brand new Soyuz launch facility in Korou, French Guyana. If ESA /Ariane wont play ball, Brazilians would be more than happy I think . Time to ask them to put money where the mouth is and ask them to back up that South-South co-operation rhetoric with substance.
The largest ethnic group is that of the descendants of indentured labourers from India also known as East Indians (Indo-Guyanese), comprising 43.5% of the population in 2002.
I completely agree..... make a 4-6 tonne GTO capable launcher and i am fine with the loss of 100-200 Kg due to launch site issueTSJones wrote:I'm not sure what you guys are expecting to benefit for having a launch site near the equator? For instance, the US has the cape in florida. It's OK but it is still a long ways from the equator. We're happy with it. Suits us fine. Our other major base is just north of Los Angelos at Vandenberg AFB. We use it for polar orbits. Fine and dandy right?
We'll not exactly. Our partners for the ISS, Russia, has to launch northeast over Siberia due to its neighbor China which is due east of Kazakistan. That means any launches that the US wants to do to the ISS must launch from the cape directly northeast along the US Atlantic sea coast in order to track the russian orbit inclination. Sucks, huh?
Well not that much really. It's been calcualted the shuttle only lost 7% payload capacity for havng to launch northeast from the cape. Not that much is it?
So again I must ask, what benefits exactly do you expect for launching near the equator?