Optimisation Study of a Homogeneously-Catalysed HTP Rocket Engine

Details Optimisation Study of a Homogeneously-Catalysed HTP Rocket Engine Optimisation Study of a Homogeneously-Catalysed HTP Rocket Engine

Oct 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004esasp.557e...9m&link_type=abstract

Proceedings of the 2nd International Conference on Green Propellants for Space Propulsion (ESA SP-557). 7-8 June 2004, Chia Lagu

Computer Science

Scientific paper

The decomposition of hydrogen peroxide (HTP) using a liquid catalyst offers an alternative to the employment of traditional catalyst packs. A test rig has been used to estimate the length of chamber required for complete decomposition to take place for the case of HTP with a phosphorus content some 10000 times the level normally associated with rocket-grade HTP. Complete decomposition within a 10 mm advection length was achieved.

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