The up-rated version of the Vikas engine tested yesterday developed a chamber pressure of 58.5 bar against 52.5 bar in the current version. This new engine uses UH25 (a mixture of Unsymmetrical Di-methyl Hydrazine and hydrazine hydrate) as fuel and nitrogen tetroxide as oxidiser. A number of short duration tests of the up-rated version had been conducted in the past few months to check the inter-play of various parameters to ensure a stable combustion before conducting the test yesterday. In addition to the verification of performance of the engine for full duration, the test has also validated the Silica-phenolic throat for the extended duration of burning time. The quick look data has indicated normal performance of the engine.

After completion of qualification, the new up-rated Vikas engine is planned to be introduced in the second developmental test flight of GSLV, which is scheduled during 2002. The new engine has the potential to increase the payload capability of GSLV by about 150 kg in the Geo-synchronous Transfer Orbit (GTO).