DocumentCode
165646
Title
MEMS microthrusters with nanoenergetic solid propellants
Author
Puchades, Ivan ; Hobosyan, Mkhitar ; Fuller, Lynn F. ; Liu, Frank ; Thakur, Siddharth ; Martirosyan, Karen S. ; Lyshevski, Sergey E.
Author_Institution
Dept. of Electr. & Microelectron. Eng., Rochester Inst. of Technol., Rochester, NY, USA
fYear
2014
fDate
18-21 Aug. 2014
Firstpage
83
Lastpage
86
Abstract
Solid propellants are used in various flight and underwater systems as well as in propulsion platforms. Micromachining, microelectromechanical systems (MEMS) and automatic dispensing of high-energy-density nanoenergetic materials are examined for current and next generation of application-specific flight and underwater platforms. The integrated MEMS-technology microthrusters with the optimized-by-design nanostructured propellants ensure the expected thrust-to-weight and thrust-to-power ratios, specific impulse, effective exhaust velocity, thrust, energy density, controlled combustion, etc. The flight-proven propulsion and micromachining technologies are suitable in a wide range of applications, such as payload delivery, stabilization, guidance, navigation, etc. Compared with mono- and bi-propellant, ion, laser, plasma, Hall-effect and other thrusters, our solution ensures fabrication simplicity, affordability, robustness, integration, compatibility, safety, etc. The experimental substantiation, evaluation and characterization of fabricated proof-of-concept devices with nanoenergetic propellants are reported.
Keywords
aerospace propulsion; marine propulsion; micromachining; nanostructured materials; propellants; Hall-effect; automatic dispensing; bi-propellant; controlled combustion; effective exhaust velocity; energy density; flight systems; flight-proven propulsion; high-energy-density nanoenergetic materials; integrated MEMS-technology microthrusters; ion; laser; microelectromechanical systems; micromachining technology; mono-propellant; nanoenergetic solid propellants; optimized-by-design nanostructured propellants; plasma; propulsion platforms; specific impulse; thrust-to-power ratios; thrust-to-weight ratios; underwater systems; Combustion; Heating; Micromechanical devices; Nanostructured materials; Propellants; Silicon;
fLanguage
English
Publisher
ieee
Conference_Titel
Nanotechnology (IEEE-NANO), 2014 IEEE 14th International Conference on
Conference_Location
Toronto, ON
Type
conf
DOI
10.1109/NANO.2014.6968072
Filename
6968072
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