ISRO - General Discussions

There are three variants it seems. 30 Ton maybe with 4 SLBs.
Yes,There are 3 variants
1. Soorya-core alone - 20T LEO
2.Soory-heavy with 2 SRBs- 30T LEO
These 2 designs are finalised
3.Soorya-super heavy with 2 Liquid boosters (similar to Falcon heavy & Longmarch-10) - 70T to LEO for manned moon mission, still under conceptual study phase
 
Yes,There are 3 variants
1. Soorya-core alone - 20T LEO
2.Soory-heavy with 2 SRBs- 30T LEO
These 2 designs are finalised
3.Soorya-super heavy with 2 Liquid boosters (similar to Falcon heavy & Longmarch-10) - 70T to LEO for manned moon mission, still under conceptual study phase
Which liquid boosters? Those SCE-200s or new methane engines, eitherway clustering will be required, I hope they bump up s200 to a new s450 level or with clustering sce-200 reach close to rd-170, but that is another monster, it uses only single turbine to generate that much power.
 
Which liquid boosters? Those SCE-200s or new methane engines, eitherway clustering will be required, I hope they bump up s200 to a new s450 level or with clustering sce-200 reach close to rd-170, but that is another monster, it uses only single turbine to generate that much power.
LOX-Methane boosters powered by 9 LME-1100 engines
 

A respected, knowledgeable commentor has called this launch hype and rubbish. Given the number of start ups claiming things, you could understand his disdain. But what about the huge number of payloads( pico sats) on board the rocket? Would this give a certain respectability to the mission? Also, the hybrid character of the propellant.
 
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Two URSC patents related to spacecraft capturing mechanisms for On-Orbit Satellite Servicing.

1) Short description of invention : Liquid Apogee Motor (LAM) Throat Capturing and Preloading (LTCP) mechanism for On-Orbit Servicing (OOS) to extend the life of non-cooperative spacecraft in LEO or GEO nearing end-of-life.
20240904_210317.jpg
2) Short description of invention : Launch Adapter Ring (LAR) Grasping and Preloading Mechanism (GPM) for On-Orbit Servicing (OOS) to extend the life of non-cooperative spacecraft in LEO or GEO nearing end-of-life. With a lightweight design under 2 kg, the GPM can handle client spacecraft weighing up to 1.5 tons. Its compact gripper reduces overall system mass and complexity, making it suitable for various applications, including refueling defunct spacecrafts and performing berthing operations on the Indian Space Station.
H3794R1.jpegaiXrQMF.jpeg
 
Two URSC patents related to spacecraft capturing mechanisms for On-Orbit Satellite Servicing.

1) Short description of invention : Liquid Apogee Motor (LAM) Throat Capturing and Preloading (LTCP) mechanism for On-Orbit Servicing (OOS) to extend the life of non-cooperative spacecraft in LEO or GEO nearing end-of-life.
View attachment 8451
2) Short description of invention : Launch Adapter Ring (LAR) Grasping and Preloading Mechanism (GPM) for On-Orbit Servicing (OOS) to extend the life of non-cooperative spacecraft in LEO or GEO nearing end-of-life. With a lightweight design under 2 kg, the GPM can handle client spacecraft weighing up to 1.5 tons. Its compact gripper reduces overall system mass and complexity, making it suitable for various applications, including refueling defunct spacecrafts and performing berthing operations on the Indian Space Station.
View attachment 8452View attachment 8453
I can see Space based ASAT here, capture enemy satellite & deorbit it, especially LEO based Reconsats
 

"There Were Lots Of Attempts...": ISRO Chief To NDTV On Cyber Fraud​

ISRO chief Dr S Somanath laid the foundation stone of a cybersecurity facility called 'Cyber Nalanda' in Bengaluru. It is the brainchild of SISA, a global forensics-driven cybersecurity solutions company​

 

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