Chandrayaan-2 : Updates

you are assuming that the speculated sections are confirmed. That has to be left to them. Besides, a technical win is a consolation prize, we need the big prizes and do it well.
Refer to my all posts which say only to wait for confirmation from official PRO. Only thing I have said confirmed is ISRO Chief statement on location of lander and trying to communicate with it. Thank you.
 
I don't know why we even consider bringing pataal-lok into discussion. They are not even in the picture just trying to take some publicity that they also have some space mission, oh la la cheering girls in the stadium that's their aukaad. We should compete with the Chinese. Ignore the pataalis.
Kya baat hai? Poore Mood Mai Ho Bajuwalon 🐷🐷 ki Lene Mai..😁
 
ok guys, confirmation that the landing was not as soft as intended. if something is working, maybe they can get it on. We will just have to wait for now.

Vikram located on lunar surface, did not soft-land: ISRO

After watching isro's animation for vikram lander many times, I wondered if it has shock absorbers for contingency. Then I said to myself that it's redundant and will only increase load. Animation shows lander have sensors in landing legs and thus restricting g forces experienced by it.
 
The Rough braking should have ended Earlier and the Fine Braking should have begun Earlier

That is the Velocity of Descent should have been Further Reduced and controlled
Much earlier

That would have given us more time to
Re establish Communication

Once it Thudded on the Surface , Communication could not be Re established
 
After watching isro's animation for vikram lander many times, I wondered if it has shock absorbers for contingency. Then I said to myself that it's redundant and will only increase load. Animation shows lander have sensors in landing legs and thus restricting g forces experienced by it.

The mass of vikram lander (including the rover inside) is 1471 kg. This article says it has shock absorbers.

Vikram has four legs and possibly may not find a totally flat location to land. But, it has an adequate mechanism to project any vibrations while landing, like the presence of shock absorbers.

Not sure if the 'shock absorbers' are the legs of lander or something more.
 
The only factor ISRO engineers and scientist miscalculated in understanding the effect of firing maneuvering thursters on the 1.4 ton Lander was moon's Gravity as well as the shifting Center of Gravity of the Lander itself with depleting fuel and the speed of angular descent.

They probably missed some factors in applying the PID control theory which resulted in too many extreme maneuvers in short intervals making the Lander lose its orientation and turn sideways and finally upside down. Moment it went upside down, the communication snapped and the main speed breaker thursters instead of slowing the Lander, acted reversely to accelerate the spacecraft towards the moon's surface.

In it's next attempt, ISRO should bring down the speed to Zero to hover at 2 km above the ground level for few seconds without any sideways maneuvers irrespective of how much ever it is off the planned trajectory, and then allow the Lander to recalculate new descend parameters towards the destination as well as have sensors to look for obstructions if any, in which case plan a round-about descend. Also, they should add redundant TR modules and additional cameras with independent battery packs which can communicate with the Orbiter, besides the main TR Communication pack.

Since the Orbiter has life of over 7 years, they can now only send the Lander for which they probably can do it on an extended version of PSLV or for sure on GSLV Mk II instead of Mk III
 
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Kya baat hai? Poore Mood Mai Ho Bajuwalon 🐷🐷 ki Lene Mai..😁

I honestly say what the f*** is Pakistan what's their achievement in space, except for watching moon and celebrating Eid that too without being sure about the moon phase. Discussing Pakistan with respect to space missions is like insult to commonsense.
 
The mass of vikram lander (including the rover inside) is 1471 kg. This article says it has shock absorbers.

On moon somewhat less than 1471kg

The only factor ISRO engineers and scientist miscalculated in understanding the effect of firing maneuvering thursters on the 1.4 ton Lander was moon's Gravity as well as the shifting Center of Gravity of the Lander itself with depleting fuel and the speed of angular descent.

No they calculated everything right. Even a class 11th student will have this parameter in mind.

They probably missed some factors in applying the PID control theory which resulted in too many extreme maneuvers in short intervals making the Lander lose its orientation and turn sideways and finally upside down

Everything was perfect, the only thing which was not perfect is the mapping. As I said the contact was lost few thousand meters above the actual landing zone, this means it landed hard because some surface suddenly appeared close ' terrain terrain' due to automated change in trajectory to find suitable place to land.

There is no reason other than false mapping to suddenly change the trajectory land 500m before and few thousand meters above the landing zone .
 
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If we have fuel remaining onboard in the lander, we can probably fire the relevent engines and try and make it upright if it is tilted. But if it has landed upside down, there is nothing much that we can do.