Skip to main content
Log in

Electro-thermal analysis of an Al–Ti multilayer thin film microheater for MEMS thruster application

  • Technical Paper
  • Published:
Microsystem Technologies Aims and scope Submit manuscript

Abstract

A multilayer thin film aluminum/titanium (Al/Ti) microheater is developed for the microthruster liquid propellant vaporizing and gas heating for increasing the specific impulse. The microheater was fabricated onto a Pyrex 7740 substrate using a Micro-Electro-Mechanical Systems processing technology. A finite-element based multiphysics simulation was employed to simulate the microheater performance. The distribution of temperature and variation of the thermal deformation are simulated in modeling with the different input power. And the simulation shows that heat loss of the microheater is relatively low comparing with the normal heater. Subsequently an experimental testing of the microheater performance based on infrared imaging device was actualized with applied voltage from 5 to 36 V. An auger electron spectroscopy detection was employed to validating the assumption that Al layer oxidizing is the main reason of temperature higher in the test than simulation.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14
Fig. 15

Similar content being viewed by others

Abbreviations

ρ :

Material density

q :

Heat flux tensor

C p :

Heat capacity at constant pressure

k :

Thermal conductivity

Q ted :

Thermo elastic damping

d s :

Thin layer thickness

q s :

Thin layer heat flux tensor

k s :

Layer heat transfer coefficient

V :

Potential difference

σ:

Conductivity

J e :

External current density tensor

Q j :

Current source

T :

Temperature

References

  • Cahill DG, Goodson K, Majumdar A (2014) Thermometry and thermal transport in micro/nanoscale solid-state devices and structures. J Heat Transf 124(2):222–241

    Google Scholar 

  • Cheah KH, Kai SK, Chiang CL, Chin JK (2011) Progress on development of Al2O3–SiO2 ceramic MEMS-based monopropellant micropropulsion system. In: 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Joint Propulsion Conferences. https://doi.org/10.2514/6.2011-5923

  • Chen G (2013) Thermal conductivity and heat conduction in nanostructures: modeling, experiments, and applications. In: AIAA thermophysics conference, vol 504, pp 416–420

  • Cofer AG, O’Neill WJ, Heister SD, Alexeenko A, Cardiff EH (2015) Film-evaporation MEMS tunable array for low-mass SmallSat propulsion: design improvements and thrust characterization. In: 51st AIAA/SAE/ASEE joint propulsion conference, AIAA propulsion and energy forum (AIAA 2015–3993). https://doi.org/10.2514/6.2015-3993

  • Dolci S, Dell’Amico DB, Pasini A, Torre L, Pace G, Valentini D (2015) Platinum catalysts development for 98% hydrogen peroxide decomposition in pulsed monopropellant thrusters. J Propuls Power 31(4):1204–1216

    Article  Google Scholar 

  • Fecht HJ, Friedberger A (2011) Microthruster with integrated platinum thin film resistance temperature detector (RTD), heater, and thermal insulation. In: Proceedings of SPIE—The International Society for Optical Engineering, vol 8066(1), pp 806604–806604-7

  • Haynes WM (2017) CRC handbook of chemistry and physics. CRC Press

  • Kundu P, Bhattacharyya TK, Das S (2014) Electro-thermal analysis of an embedded boron diffused microheater for thruster applications. Microsyst Technol 20(1):23–33

    Article  Google Scholar 

  • Lee J, Kim K, Kwon S (2010) Design, fabrication, and testing of MEMS solid propellant thruster array chip on glass wafer. Sens Actuators A 157(1):126–134

    Article  Google Scholar 

  • Louisos WF, Hitt DL (2008) Viscous effects on performance of two-dimensional supersonic linear micronozzles. J Spacecr Rockets 45(4):706–715

    Article  Google Scholar 

  • Mirmira SR, Fletcher LS (1998) Review of the thermal conductivity of thin films. J Thermophys Heat Transf 12(12):121–131

    Article  Google Scholar 

  • Seo D, Lee J, Kwon S (2012) The development of the micro-solid propellant thruster array with improved repeatability. J Micromech Microeng 22(9):094004

    Article  Google Scholar 

  • Tanaka S, Kondo K, Habu H, Itoh A, Watanabe M, Hori K, Esashi M (2008) Test of B/Ti multilayer reactive igniters for a micro solid rocket array thruster. Sens Actuators A 144(2):361–366

    Article  Google Scholar 

  • Torre FL, Kenjereš S, Moerel JL, Kleijn CR (2011) Hybrid simulations of rarefied supersonic gas flows in micro-nozzles. Comput Fluids 49(1):312–322

    Article  MathSciNet  MATH  Google Scholar 

  • Zhang KL, Chou SK, Ang SS (2004) Development of a solid propellant microthruster with chamber and nozzle etched on a wafer surface. J Micromech Microeng 14(6):785–792

    Article  Google Scholar 

  • Zhang KL, Chou SK, Ang SS (2007) Fabrication, modeling and testing of a thin film Au/Ti microheater. Int J Therm Sci 46(6):580–588

    Article  Google Scholar 

Download references

Acknowledgements

This work is supported by the Major Program of National Natural Science Foundation of China under Grant numbers 61690210 and 61690213.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Xiaoqian Chen.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Li, X., Huang, Y., Chen, X. et al. Electro-thermal analysis of an Al–Ti multilayer thin film microheater for MEMS thruster application. Microsyst Technol 24, 2409–2417 (2018). https://doi.org/10.1007/s00542-017-3649-5

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s00542-017-3649-5

Navigation