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- Apr 29, 2015
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New Indian company called EtherialX
Proposes a larger HLV (much bigger than Delta-IV & Proton-M) with:
24.8 tonnes to LEO
20.8 tonnes to GEO (direct)
6.8 tonnes to TLI (Trans-lunar injection)
(Screenshot from website)
Later both require a powerful upper-stage which has only been available with US, USSR and China till date and hasn't been realised even by ISRO till date.
And all of this going to be re-usable too!
925 kN
Propellant
RP1/LOX
Feed Cycle
Gas Generator
Isp (Sea Level)
~275s-295s
Isp (Vacuum)
~313s-330s
EtherealX
www.etherealx.space
Proposes a larger HLV (much bigger than Delta-IV & Proton-M) with:
24.8 tonnes to LEO
20.8 tonnes to GEO (direct)
6.8 tonnes to TLI (Trans-lunar injection)
(Screenshot from website)
Later both require a powerful upper-stage which has only been available with US, USSR and China till date and hasn't been realised even by ISRO till date.
And all of this going to be re-usable too!
Razor Crest Mk-1
Introducing India’s and the world's most powerful partially reusable vertical landing medium-lift launch vehicle yet.
EtherealX Stallion
ThrustThe EtherealX Razor Crest Mk-1 will house 9 of the most powerful operational liquid rocket engines in all of Asia, Europe, Australia, Africa, South America, and Antarctica - Stallion. EtherealX's single Stallion engine will be capable of producing an enormous 925 kilonewtons of thrust, enabling the Razor Crest Mk-1 to carry 20 tonnes to LEO. Making it one of the most powerful to-be operational medium-lift reusable vertical landing launch vehicles ever. Razor Crest will be established as the workhorse of India and will inevitably result in revolutionary beginnings for in-space services and human spaceflight programs.
925 kN
Propellant
RP1/LOX
Feed Cycle
Gas Generator
Isp (Sea Level)
~275s-295s
Isp (Vacuum)
~313s-330s