- Joined
- Jul 1, 2024
- Messages
- 841
- Likes
- 1,860
30ton LEO Soorya is not base variant, it's the heavy variant, base variant i.e SOORYA-CA has 20ton LEO, while SOORYA-H has 30ton LEO
You sure?
30ton LEO Soorya is not base variant, it's the heavy variant, base variant i.e SOORYA-CA has 20ton LEO, while SOORYA-H has 30ton LEO
YesYou sure?
There are three variants it seems. 30 Ton maybe with 4 SLBs.30ton LEO Soorya is not base variant, it's the heavy variant, base variant i.e SOORYA-CA has 20ton LEO, while SOORYA-H has 30ton LEO
One more how they collect the stage to reuse it ? No details about itWasn't this launch from early 2023
And those two-three competitors outrage us by a huge mile or more. Still a low bar.We only have 2-3 real competitors out of nearly 200 countries in future anyway.
Yes,There are 3 variantsThere are three variants it seems. 30 Ton maybe with 4 SLBs.
Most likely parachuteOne more how they collect the stage to reuse it ? No details about it
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.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
LOX-Methane boosters powered by 9 LME-1100 enginesWhich 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.
That's one version, there's another larger version with more propellant loading under conceptual study phaseWiki says up to 49 tons.
I can see Space based ASAT here, capture enemy satellite & deorbit it, especially LEO based ReconsatsTwo 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