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Nilgiri

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The docking may be attempted a few more times, but it may be delayed till March:

 

Gessler

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Let's goooo!


This is a crucial step to prove for the upcoming Chandrayaan-4 sample return mission which would involve a lot of docking & un-docking! Not to mention, a scaled-up version will go on our Space Station as well.

Btw, our docking mechanism is meant to be compatible with the NASA/ISS standard so possibility of international collaboration would also be open.
 

kakaliam2

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Let's goooo!


This is a crucial step to prove for the upcoming Chandrayaan-4 sample return mission which would involve a lot of docking & un-docking! Not to mention, a scaled-up version will go on our Space Station as well.

Btw, our docking mechanism is meant to be compatible with the NASA/ISS standard so possibility of international collaboration would also be open.
I wonder would this docking be rudimentary compared to pressurised Vehicle docking like we seen in Crewed Modules? Or is it something depends entirely on Module itself?
 

Nilgiri

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I wonder would this docking be rudimentary compared to pressurised Vehicle docking like we seen in Crewed Modules? Or is it something depends entirely on Module itself?

I would say the main technologies involved (sensoring, precise control and maneuver) are now proven.

Pressurized docking would just need confirmation of perfect seal for an air lock. If that wasn't validated this time, it shouldn't be too difficult for a future mission that scales what was proven here.
 

Saithan

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@Saithan thanks for all the likes, you saw the mission in accelerated format on your end 🤣
Oh yes, and the progress made is very impressive, especially what was achieved in 2024. A lot of work and planning was put into this and to succeed without fail is testament to how dedicated and competent the people in these projects are 😄
 

kakaliam2

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This restart capability is for ADMIRE Program to demonstrate VTVL.

On a broader note, it seems the Indian Space Industry unlike the MIC doesn't suffer from any penny pinching or short-term band aid solutions. The first steps were hard, but moving on and on akin to a snowball effect their capabilities are growing larger, the last 5 years were significant.
 

Nilgiri

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The Liquid Propulsion Systems Centre of ISRO dispatched the Crew Module for the first uncrewed mission of Gaganyaan (G1), the space agency said on Wednesday. The dispatch occurred after the complete integration of the liquid propulsion system.


ISRO plans to send an uncrewed mission to space before launching the crewed mission under its Gaganyaan project, marking the first step toward acquiring human spaceflight capabilities.


“On 21 January 2025, the Liquid Propulsion Systems Centre (LPSC) of ISRO dispatched the Crew Module for the first uncrewed mission of Gaganyaan (G1), after successfully completing the integration of the liquid propulsion system,” ISRO said in a statement.


LPSC, Bengaluru has dispatched the module to Satish Dhawan Space Centre, Sriharikota, officials said.

The Crew Module Propulsion System (CMPS), designed for precise three-axis control—Pitch, Yaw, and Roll—of the crew module, is a key component of the mission. This bi-propellant-based Reaction Control System (RCS) will be activated after the separation of the service module during the descent and re-entry phase, continuing until the parachute-based deceleration system is deployed.


“The system uses 12 100N thrusters, a pressurization system with high-pressure gas bottles, and a propellant feed system, along with the associated fluid control components,” an ISRO spokesperson said.


The 100N thrusters are rocket motors used in spacecraft for propulsion. Additionally, the Crew Module Uprighting System (CMUS), developed by the Vikram Sarabhai Space Centre (VSSC), was integrated into the module at LPSC.

ISRO also stated that the Crew Module will undergo further integration processes, including avionics package assembly, electrical harnessing, and checks at VSSC. Following this, it will be dispatched to the U R Rao Satellite Centre in Bengaluru for the final integration phase of the Orbital Module.


(With PTI Inputs)
 

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