SCE-200
The SCE-200 is an Indian, under-development, liquid-fuel rocket engine, burning liquid oxygen (LOX) and RP-1 kerosene in an oxidizer-rich staged combustion cycle. This engine is expected to power Indian Space Research Organization's upcoming Unified Launch Vehicle (ULV) and Reusable Launch Vehicle (RLV). It is being developed by the Liquid Propulsion Systems Centre, a subsidiary of ISRO. But before that it will be tested on a GSLV Mk III by replacing the L110 stage powered by the Vikas engine with an SC-200 stage powered by SCE-200 engine and a 200 tonne propellant load.
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SCE-200
The SCE-200 is an Indian, under-development, liquid-fuel rocket engine, burning liquid oxygen (LOX) and RP-1 kerosene in an oxidizer-rich staged combustion cycle. This engine is expected to power Indian Space Research Organization's upcoming Unified Launch Vehicle (ULV) and Reusable Launch Vehicle (RLV). It is being developed by the Liquid Propulsion Systems Centre, a subsidiary of ISRO. But before that it will be tested on a GSLV Mk III by replacing the L110 stage powered by the Vikas engine with an SC-200 stage powered by SCE-200 engine and a 200 tonne propellant load.
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The SCE-200 is an Indian, unde ...... d a 200 tonne propellant load.
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Wikipage page ID
44,981,458
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1,012,251,846
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combustion chamber
country of origin
dry weight
~2700 kg
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fuel
manufacturer
Godrej Aerospace, Godrej & Boyce Ltd
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mixture ratio
name
SCE-200
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oxidiser
purpose
Main engine
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status
Under Development
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throttle range
type
liquid
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wikiPageUsesTemplate
subject
hypernym
type
comment
The SCE-200 is an Indian, unde ...... d a 200 tonne propellant load.
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label
SCE-200
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