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CE-7.5 Indian cryogenic rocket engine The Cryogenic Upper Stage has the following specifications: 1. Operating Cycle - Staged combustion 2. Propellant Combination - LOX / LH2 3. Thrust Nominal (Vacuum) - 75 kN 4. Operating Thrust Range - 73.55 kN to 93.1 kN (To be set at any fix values) 5...

Re: India's GSLV successfully launched GSAT-14 :cb: :cheer2: :high5: :whoo: :bhangra: :rock: :gangnam:

After this launch ISRO scientists should also develop rockets of Saturn V category. Nothing is impossible.

HOORAY!! Next Stop India's manned mission to space.