This is an awesome and brilliant application of Computational Origami, a very lesser known subfield of Computational Geometry. I did my Masters' Research Project on this topic in my institute. In my final semester I will be continuing on this topic's application in proteins and finally complete the entire project.
Good that they're experimenting different things. It doesn't matter if it's feasible, until you try you cannot determine the results so it's very pleasant to see ISRO making new things which we had never tried before. If it's a success then great, if not still great try!! ❣️🇮🇳
Nice to see such wonderful progress on R&D. We're working on Light Weight Solar Sail based on Flexible Robotics. It's good to learn from your channel always.
I think isro will change the gas used from nitrogen to helium or something else in later stages and thickness and design of the dragchute will be changed to something like a pointed shroom... but it`s a pretty solid concept...
Drone net is incredible idea. I can imagine drone net with integrated parachute.. this will not only avoid heavy parachute in the space craft but also make the payload recoverable
@@debanjansaha1304 You don't have to carry heavy parachutes using precious rocket fuel and space within the aircraft. The parachute deployment system also adds to the weight and complexity.
Bro got question, will ISRO make rocket similar to ULA Vulcan. Because Vulcan rocket is combination of Altas 400 series + 500 series and Delta IV. Which is huge cost saving with single rocket model and highly customizable.
looks very sophisticated and nerve wreaking particularly the drone part, I am thinking if we can burst another inflatable just before splash held by long unwinding thread
Please make a video about Aditya L1 mission, I am in IIA and IIA is making VELC payload for the mission. This is going to be a very ambitious mission, this is better then almost all of the current solar CORONAGRAPHS like SDO.
A small step before the giant leap, no doubt. Bhai, most of these experiments are replications or lower-cost improvements of what has already been done by the NASA / Roscosmos / ESA / Chinese / Japanese / SpeceX, etc. Have we (ISRO) performed any manoeuvre or made any component that is truly unique, which has opened up newer possibilities in rocketry and space research ? Thanks.
Almost all of chandrayaan 2 experiments like DFSAR, OHRC, XSM, and others are world class never before seen standards Similarly upcoming nisar, chandrayaan 3, shukrayan, etc
Any reason why they didn't use a chemical gas generator (eg. Sodium Azide or Hydrogen Peroxide) instead of nitrogen in a tank? Wouldn't it be a more efficient way to store the same quantity gas required?
For the re-entry of interplanetary / orbital probes, the idea is certainly excellent. But the stage re-entry, in recyclable condition, is not very good. control systems are now very accurate and may well "land" on a trampoline (no chassis needed!), near the launch complex. Integral/"package" TSTO layout, as on P-7. In its further evolutionary development. only boosters B, V, G, D become panels, a kind of "surfboards". Being parts of a generatrix of a common cone. Without central block "A". each "board" has its own control system, 3 liquid rocket engines Control systems are now very accurate and may well "land" on a trampoline (no landing gear’s ), near the launch complex. If anyone is interested I will continue
Sir agar hum parashut ke jagh wing ka use Kare ,jaise helicopters flying ka principal ke hisabse agar wing sahiangle Mai rahte hai to helicopters ak jaghpe stady raheta hai isi tarahase friction Kam hotel hooye sahi jaghpe land karega
It's main glory is for interplanetary missions. For example, nasa is developing HIAD (Hypersonic Inflatable Aerodynamic Decelerator) for future mars missions because using a heavy ceramic heat shield is not a good idea.
Hi This is Abhijeet Deshpande and the Nitrogen cooled inflatable heat shield was proposed by me to NASA for its James Webb Space Telescope as an integrated disposable attachment for the James Webb Space Telescope to rotate on its axis without compromising on the telescopes ability to utilize its potential even during axis rotation. The Disposable nitrogen cooled inflatable heal shield was supposed to be launched in space with my MAD CAPS Drones - a concpet which I have copyrighted and proposed to all space agencies as well. i.e. Maintenance Assistive Drone Capsules - which would have robotic appendages including welding and removal tools for insertion and welding into the James Webb Space Telescope as a disposable telescope appendage. This was almost four years ago. Anyways, amongst many others.....👍
Agar IAD thin atmosphere mtlb higher altitude me inflate hoga, toh niche aate aate uska pressure decrease nhi hojayega?? Tb toh saggy ho jayega shayad. I can be wrong. So correct me. Thanks
Bhaiya pls explain that How we will locate that capsule If it not landed to the marked location or is there past incident of any mission in which the capsule got missed ? 🤔 just for curiosity .
This technology is applicable in landing on celestial bodies with atmosphere and best, but for celestial bodies without atmosphere retro propulsion or magnatic levitation willbe applied out of these two retro propulsion appears to be best at present.
If we just want to slow it down when it is falling (what i understood may i am wrong) then why don't we just give some short fire boost to upside for bringing it at velocity zero
Because that would require fuel which would increase weight which would also increase rentrty velocity. And no a 'small' boost can't cut it then in that small space
WHAT WOULD HAPPEN IF THIS WERE FILLED WITH HELIUM OR HYDROGEN IN STEAD OF NITROGEN ? 🤔 CAN YOU SIMULATE THAT? WOULD THAT HELP IN SLOWING THE VEHICLE BETTER ON RENTRY ?
@@GareebScientist ok, they will use this heatshield for gslv also but that velocity of that stage will be higher and after return they need a new IAD for another reusable flight , will it be economical ?
Reuable rocket is the need of isro. Crashlandings happen in its devlopment but failure is a step towards it. Just need courage to do some fail projects which looks difficult with isro.
Bro with honest don't u think isro's speed in terms of innovation as a psu is too slow.I am so optimistic about it but when I see small start up r taking over the market .it's leads me to think what r the scientist actually doing, does they really working or just coping from another (like coping from Ukranian engine)why we couldn't develope our own engine when we r expecting to atmanirbhar
@@GareebScientist i'm talking about the commercial lunch market. Companies like rocket labs,Ula,Astra space and even small start ups that r Not even having the require funds to have employees and almost leading to bankrupt r innovating reusable rocket technology rapidly.And it's clear that we r much more away from that, and why isro's speed is too slow when having a secure source of fund.Not even able to develope an indigenous semicryo engine its look like pocketry not rocketry and instead of just hyping we should focus on using isro's real potential .
Bhaiya use glide bhi to kar sakte hai and tail fins se control karke chote wheels side pe laga kar just land like jo vo glide suit hota hai vesa vala no need of propalsion just one tail fin with pitch and yo control (bad spelling 😅) bahiya response karna
controlling drone to carry a flying net need some practice, do they practice it already? If no, then easy way is just reduce payload capacity in exchange for a parachute or wings, and then hire a boat to recover them at sea.
@@gen-z-box3331 no need to program a computer, just hire drone pilots to carry the net, what use of India's pilot if everyone only want to ask for a robot.
Why does ISRO trying to catch or slow down rocket using drones and net. Shouldn't using large parasuits be enough to land them safely, in the same way Astronauts in capsules land on Earth
@Gareeb Scientist In the wake of China's demonstrated capability to target other nation's satellites, could you please research and make a video about what, if any, has been India's response to this (other than demonstrating similar capability ourselves, which India did demonstrate a couple of years back following China's demonstration)? I am thinking more in the lines of giving each satellite intelligence to move away (temporarily) from the path of the enemy projectile (perhaps going out of service temporarily, so as to survive and come back in service later). What, if any, could be the challenges to such manoeuvres (high speed approach of the enemy projectiles, high power requirements for constantly looking out for enemy projectiles, etc.). Are other countries known to have such enemy projectile dodging capabilities?
Really happy that ISRO is moving to reusable spacecrafts, extremely interesting idea. I just wish that they interact with the masses more :(
Human missions are best to do so. Wait for it bro.
Hope they do exceptional PR work and outreach for Gaganyaan G1 crewed mission
Are you studying engineering in Bangalore by chance ??
This is an awesome and brilliant application of Computational Origami, a very lesser known subfield of Computational Geometry. I did my Masters' Research Project on this topic in my institute. In my final semester I will be continuing on this topic's application in proteins and finally complete the entire project.
@@Parrot3054 Let's just say our interests are similar :)
cool! protiens?
@@GareebScientist Yes related to protein folding, which is a huge domain in itself
Very nice CGI graphic!! When will it be happened!?
This can be the game changer for Indian commercial space industry. ISRO rocks.
Good that they're experimenting different things. It doesn't matter if it's feasible, until you try you cannot determine the results so it's very pleasant to see ISRO making new things which we had never tried before. If it's a success then great, if not still great try!! ❣️🇮🇳
True
Nice to see such wonderful progress on R&D. We're working on Light Weight Solar Sail based on Flexible Robotics. It's good to learn from your channel always.
ISRO ♥️♥️♥️♥️♥️♥️
Too good. Happy to see innovative approach in recovery. Mainly the drone net is really intriguing
I think isro will change the gas used from nitrogen to helium or something else in later stages and thickness and design of the dragchute will be changed to something like a pointed shroom... but it`s a pretty solid concept...
Drone net is incredible idea. I can imagine drone net with integrated parachute.. this will not only avoid heavy parachute in the space craft but also make the payload recoverable
Thanks.... I could not understand why this thing is superior to parachute.
@@debanjansaha1304 You don't have to carry heavy parachutes using precious rocket fuel and space within the aircraft. The parachute deployment system also adds to the weight and complexity.
ISRO is my dream ❤️❤️❤️
Bro got question, will ISRO make rocket similar to ULA Vulcan. Because Vulcan rocket is combination of Altas 400 series + 500 series and Delta IV. Which is huge cost saving with single rocket model and highly customizable.
You are legend Bhaiya. Lots of love from Uttarakhand.
Bhai regular video bnaya kro... Eagerly wait for your videos
Appreciate your efforts brother 🔥
looks very sophisticated and nerve wreaking particularly the drone part, I am thinking if we can burst another inflatable just before splash held by long unwinding thread
This Chanel deserve more more and more likes.
I'm a aerospace final year , I'm currently working on such high speed decelerators. we are developing one for 5kg lander on mars
All the best! Would love to know more. Any paper or anything?
Awesome bro any updates ?
Where are you studying?
We are so proud of our ISRO's Genius Scientists Jai Hind vande matrbhume Jayatu jayatu Bharatam
Bhaiiya reusable rockets test lr rha tha isro, ky update hai ab uska
Thanks nice information for space lovers like us 🙏🙏🥰🙏🙏
Please make a video about Aditya L1 mission, I am in IIA and IIA is making VELC payload for the mission. This is going to be a very ambitious mission, this is better then almost all of the current solar CORONAGRAPHS like SDO.
at the right time i will, will contact IIA
A small step before the giant leap, no doubt.
Bhai, most of these experiments are replications or lower-cost improvements of what has already been done by the NASA / Roscosmos / ESA / Chinese / Japanese / SpeceX, etc. Have we (ISRO) performed any manoeuvre or made any component that is truly unique, which has opened up newer possibilities in rocketry and space research ?
Thanks.
Almost all of chandrayaan 2 experiments like DFSAR, OHRC, XSM, and others are world class never before seen standards
Similarly upcoming nisar, chandrayaan 3, shukrayan, etc
@@GareebScientist 🙏🙏
Proud to be Indian ❤️🇮🇳
Eagerly waiting for GAGANYAAN 🔥🔥
Kab hai launch ?
Any reason why they didn't use a chemical gas generator (eg. Sodium Azide or Hydrogen Peroxide) instead of nitrogen in a tank? Wouldn't it be a more efficient way to store the same quantity gas required?
Is it possible to use gravity force and convert into energy which can use to control the loader ?
Your idea is right about drone (relative velocity) but how can you make the net stable .
If IAD is experimented with the design elements of dandelion seeds, the landing speed could be further reduced.
Yaar, abhi toh "Paise ki gareebi" sabse badi lag rahi hai, naahi gyaan ki gareebi! 😬
i have one suggestion can't we use a inflatable ball type structure around experiment payload. I may be wrong .
Good idea sir ji relative velocity...
Nice Video GS
Yes sir!
Could you please make video about Boinc distributed computing software, zooniverse,citizen scientist , quantum moves,foldit, folding@home etc
For the re-entry of interplanetary / orbital probes, the idea is certainly excellent.
But the stage re-entry, in recyclable condition, is not very good.
control systems are now very accurate and may well "land" on a trampoline (no chassis needed!), near the launch complex.
Integral/"package" TSTO layout, as on P-7. In its further evolutionary development.
only boosters B, V, G, D become panels, a kind of "surfboards". Being parts of a generatrix of a common cone.
Without central block "A". each "board" has its own control system, 3 liquid rocket engines
Control systems are now very accurate and may well "land" on a trampoline (no landing gear’s ), near the launch complex.
If anyone is interested I will continue
D2 ka kya scene he filhal??
December fix na?
Sir agar hum parashut ke jagh wing ka use Kare ,jaise helicopters flying ka principal ke hisabse agar wing sahiangle Mai rahte hai to helicopters ak jaghpe stady raheta hai isi tarahase friction Kam hotel hooye sahi jaghpe land karega
kya hamare isro ke pass self dock system nah nahi, consider gps/navic
It's main glory is for interplanetary missions. For example, nasa is developing HIAD (Hypersonic Inflatable Aerodynamic Decelerator) for future mars missions because using a heavy ceramic heat shield is not a good idea.
Video on ISRO HYBRID ENGINE.?
hey where can i read or know about all latest news n updates about isro n all the crazy work going on in science field???
a , isro has a reddit so all the information are the and on time so prefer ISRO subreddit or office website .
@@aniotaku2381 can't find latest updates on website....
@@tanishkaagarwal1280 Go to reddit
Hi This is Abhijeet Deshpande and the Nitrogen cooled inflatable heat shield was proposed by me to NASA for its James Webb Space Telescope as an integrated disposable attachment for the James Webb Space Telescope to rotate on its axis without compromising on the telescopes ability to utilize its potential even during axis rotation.
The Disposable nitrogen cooled inflatable heal shield was supposed to be launched in space with my MAD CAPS Drones - a concpet which I have copyrighted and proposed to all space agencies as well. i.e. Maintenance Assistive Drone Capsules - which would have robotic appendages including welding and removal tools for insertion and welding into the James Webb Space Telescope as a disposable telescope appendage.
This was almost four years ago.
Anyways, amongst many others.....👍
love you brother ❤️ like your video 😊
4:26 even for drones isn't that high speed?
Same as Vikram lander on Moon. Having landing legs and using some thrust to control landing ....
Agar IAD thin atmosphere mtlb higher altitude me inflate hoga, toh niche aate aate uska pressure decrease nhi hojayega?? Tb toh saggy ho jayega shayad.
I can be wrong. So correct me. Thanks
Hmm very intresting 😲
Gareeb bhai ne Twitter me kahan tha ki esi hafte aayega... aur aa bhi gya .. Gareeb bhai ki Jai Ho ✨🚀
Bro it's application in future me kya hai
😭I am 6 days late for video.
But good and informative video as always bhai
Bhaiya pls explain that
How we will locate that capsule If it not landed to the marked location
or is there past incident of any mission in which the capsule got missed ? 🤔
just for curiosity .
Radar and satellite navigation and tracking..
Very interesting feature.
Chandrayaan 3 me 360⁰ view camera laga hota to kitna accha hota bhaiya. Lander aur rover dono me ..🥳
this reminded me of Sea Dragon project of NASA
I thought that u were not posting any videos just yesterday
Bhai ye isro itna slow kyu ho gya hai budget problem hai kya?
48 m/s is approximately 180 km/h.
This technology is applicable in landing on celestial bodies with atmosphere and best, but for celestial bodies without atmosphere retro propulsion or magnatic levitation willbe applied out of these two retro propulsion appears to be best at present.
This is really interesting.
Can it withstand orbital re-entry?
Heat will destroy it ,as it happend to Columbia space shuttle.
Can magnets be used to cause deceleration and then collect it in drone net?
Uhh no
If we just want to slow it down when it is falling (what i understood may i am wrong) then why don't we just give some short fire boost to upside for bringing it at velocity zero
Because that would require fuel which would increase weight which would also increase rentrty velocity. And no a 'small' boost can't cut it then in that small space
WHAT WOULD HAPPEN IF THIS WERE FILLED WITH HELIUM OR HYDROGEN IN STEAD OF NITROGEN ? 🤔 CAN YOU SIMULATE THAT? WOULD THAT HELP IN SLOWING THE VEHICLE BETTER ON RENTRY ?
Hydrogen is inflammable.
Is apprenticeship in isro for 1 year worth it?
4:36 practically not possible... Drone should cover a large distance to overcome...
1:22 “Apogee” ka uchchaaran : “Apo-jee.”
Catching it through a net installed in a boat in the ocean like starlink fairing collection might be great option than that.
to land rocket proportionally they need the engines with throttling capibility..
Yes, vikas they are working on throttle
@@GareebScientist ok, they will use this heatshield for gslv also but that velocity of that stage will be higher and after return they need a new IAD for another reusable flight , will it be economical ?
Whether it will be economical that only isro can tell as they have the numbers
@@GareebScientist yes at the end of the day , ISRO can tell us.
Reuable rocket is the need of isro. Crashlandings happen in its devlopment but failure is a step towards it. Just need courage to do some fail projects which looks difficult with isro.
Nice🔥🔥🔥🔥🔥🔥🔥🔥 first comment
Bro with honest don't u think isro's speed in terms of innovation as a psu is too slow.I am so optimistic about it but when I see small start up r taking over the market .it's leads me to think what r the scientist actually doing, does they really working or just coping from another (like coping from Ukranian engine)why we couldn't develope our own engine when we r expecting to atmanirbhar
We need to give projects and technology to startups. At least 3 company with rockets will make healthy privatized launch industry.
Small startup taking over market.? Which?
@@GareebScientist i'm talking about the commercial lunch market. Companies like rocket labs,Ula,Astra space and even small start ups that r
Not even having the require funds to have employees and almost leading to bankrupt r innovating reusable rocket technology rapidly.And it's clear that we r much more away from that, and why isro's speed is too slow when having a secure source of fund.Not even able to develope an indigenous semicryo engine its look like pocketry not rocketry and instead of just hyping we should focus on using isro's real potential .
Do you think ISRO has any plans to use liquid fuel propulsion for the rocket instead of solid boosters?
They are using liquid propulsion for more than 2 decades now
Discord link plzz
Can Kevlar withstand that much of heat
Suborbital flight is not much energy, not much heat compared to orbital
I found it a complex option for payload recovery !!
Can this be used for moon or Mars landing?
Mars as a deceleration potentially yes.
You are using ksp
Booster Rocker laga do Opposite side mai jo Opposite Drag create kar k speed to slow kar dega 🤔
Weight
Bhaiya use glide bhi to kar sakte hai and tail fins se control karke chote wheels side pe laga kar just land like jo vo glide suit hota hai vesa vala no need of propalsion just one tail fin with pitch and yo control (bad spelling 😅) bahiya response karna
There are materials (cloth like ) that can resist heat (jwst me bhi use hua hai uski shield me )
Weight complexity for a very tiny stage
@@GareebScientist yaa it is but from one perspective it is saving money too. Let's see what's next
No you will limit number of experiments it can carry. In this case money isn't being saved experiments are being recovered.
I can count but I need all information
why not parachutes like others??????
Great 👌
1 liter liquid nitrogen weight is 1.782
So total liter is 236
So total weight is 420.552
it is at 1.1 bar which is not stp, and your value for 1 litre nitrogen maybe wrong
Why rockets are now looking like UFOs of film
💥💥💥
Nice👍
❤️
OP videos
Jai hind 👍
This makes SpaceX look far superior. I think using propulsion is the robust way.
controlling drone to carry a flying net need some practice, do they practice it already? If no, then easy way is just reduce payload capacity in exchange for a parachute or wings, and then hire a boat to recover them at sea.
The drones can be trained through ml for coordination along with isro might run exposed simulations
@@gen-z-box3331 no need to program a computer, just hire drone pilots to carry the net, what use of India's pilot if everyone only want to ask for a robot.
Nice
Bhai I thought channel dead
Har roz 5 bar check krta tha videio aya ya nhi 😔
Nai nai bas travel lathargy tha
👍 👍
nice
Why does ISRO trying to catch or slow down rocket using drones and net. Shouldn't using large parasuits be enough to land them safely, in the same way Astronauts in capsules land on Earth
Parachutes are heavy, will reduce payload. And this isn't for all rockets. Will know their plans with IAD over time
Gareeb bhai op 😘😘
🔝
Basically achieving what SpaceX achieved but Cheaper !
This for smaller rockets. Big rockets they are planning a SpaceX style reocevery only
Nice name
अगर आप हिंदी में बोल रहे हैं, तो आप से निवेदन है कि आप सुध्द हिंदी में ही बोले।
इससे हमे समझने में भी आसानी होगी 🙏
@Gareeb Scientist In the wake of China's demonstrated capability to target other nation's satellites, could you please research and make a video about what, if any, has been India's response to this (other than demonstrating similar capability ourselves, which India did demonstrate a couple of years back following China's demonstration)? I am thinking more in the lines of giving each satellite intelligence to move away (temporarily) from the path of the enemy projectile (perhaps going out of service temporarily, so as to survive and come back in service later). What, if any, could be the challenges to such manoeuvres (high speed approach of the enemy projectiles, high power requirements for constantly looking out for enemy projectiles, etc.). Are other countries known to have such enemy projectile dodging capabilities?