Development and Simulation of an Embedded Hydrogen Peroxide Catalyst Chamber in Low-Temperature Co-Fired Ceramics

Donald Plumlee, Judi Steciak, Amy Moll

Research output: Contribution to journalArticlepeer-review

25 Scopus citations

Abstract

Satellites in the range of 10-50 kg require small propulsion devices to perform station-keeping tasks in orbit. Low-temperature co-fired ceramic structures provide a unique platform to produce a reliable, low-cost micropropulsion system. The design uses microchannels embedded in the ceramic substrate to create a nozzle and embedded catalyst chamber. A hydrogen peroxide monopropellant is injected into a silver-coated catalyst chamber structure. The monopropellant decomposes into hot gas, which is expelled through the nozzle producing thrust. A thermal energy balance and a kinetic model is presented along with performance testing.

Original languageAmerican English
Pages (from-to)406-414
Number of pages9
JournalInternational Journal of Applied Ceramic Technology
Volume4
Issue number5
DOIs
StatePublished - Oct 2007

EGS Disciplines

  • Materials Science and Engineering

Fingerprint

Dive into the research topics of 'Development and Simulation of an Embedded Hydrogen Peroxide Catalyst Chamber in Low-Temperature Co-Fired Ceramics'. Together they form a unique fingerprint.

Cite this