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Add the following 1st stage - LM400 - 400tons of Liquid Methane/LOX propellant, powered by 9* 980KN methalox engines 2nd stage - LM120 - 120tons of Liquid Methane/LOX, powered by 2* 980KN methalox engines 3rd stage - LM40- 40tons of Liquid Methane/LOX, powered by 200KN methalox engine Payload...

MSTAR signs MoU with IN-SPACe for development of all liquid (semi-cryo) small sat LV https://m.economictimes.com/news/science/mtar-in-space-india-ink-pact-for-development-of-all-liquid-small-satellite-launch-vehicle/amp_articleshow/96172013.cms MTAR Technologies on Monday said that it has...

lack of forward thinking & money...when LPSC is constructing the Vikas engine test stand, Dr.Nambi Narayanan proposed to make it slightly larger so that they can test a 4 engined core similar to Ariane 4 core or LM-2F core, then ISRO chairman Satish Dhawan rejected that idea,later he accepted...

All 3

This is the development model for NGLV

planning stage

early 2030 I'm guessing. Also they ditched expensive Cryo upper stage. I don't think the rocket with Semi-cryo engine will achieve that $1900 target, but Methalox version may reach it

It will be jointly developed by ISRO & our Pvt companies....earlier LVs were developed solely by ISRO while private players acted as suppliers....now pvt companies will be part of design & development activities.. this new LV will replace all 3 , PSLV,GSLV & GSLV-MK3

4 or 5 ....but I'm guessing 5, because during landing you should have low thrust, if you have 5 engines,central engine can be used for landing, but if you have 4 engines, you have to use 2 engines for landing, which makes landing bit more complicated because of the extra thrust you will get...

Naacho BC :basanti::cruisin2: @Indx TechStyle @Swesh @Okabe Rintarou @omaebakabaka and others

We should develop Al-Li Alloy tanks...our payload fraction is too low