Onset voltage modeling of micromachined colloid thrusters

نویسندگان

  • Renato Krpoun
  • Herbert R. Shea
چکیده

The onset voltage of a colloid thruster is an important parameter in the design of micromachined thrusters. Because dimensions in MEMS thrusters are in the range of several tens of micrometers and because extractor electrodes can be only 5 μm from the capillary emitters, the aspect ratios for MEMS thrusters are much lower than the one of individual stainless steel or silica glass needles. Therefore the results obtained with established analytical models, that do not consider any parasitic structures, deviate significantly from experimental results on MEMS thrusters. This paper presents a new method to determine the onset voltage of micromachined colloid thrusters by combining electrostatic FEM analysis, including a model of the formation of the Taylor cone, with the equilibrium equation between electrostatic and surface tension stress. The correlation between onset voltage results obtained using the method presented in this paper and experiments are in very good agreement and validate the method for this type of microfabricated thruster.

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Progress Towards a Miniaturized Electrospray Thruster for Flexible Propulsion of Small Spacecraft

Miniaturized electrical thrusters based on electrospray (or colloid) emitters could revolutionize the spacecraft industry by providing e cient propulsion capabilities to micro and nano satellites (1-100 kg). We report on our recent advances in the development of this technology within the MicroThrust (www.microthrust.eu) European consortium. We present the design and operation of the currently ...

متن کامل

Numerical Simulation of a single emitter colloid thruster in pure droplet cone-jet mode

New Scientific missions call for emerging propulsion technologies capable of fine tuning a satellite’s relative position and cancelling small disturbances. One candidate technology that holds promise for these type of missions are colloidal thrusters. These thrusters are electrostatic accelerators which do not rely on gas ionization (plasma), are intrinsically small, and operate at low power le...

متن کامل

Hybrid-PIC modeling of a high-voltage, high-specific-impulse Hall thruster

The primary life-limiting mechanism of Hall thrusters is the sputter erosion of the discharge channel walls by high-energy propellant ions. Because of the difficulty involved in characterizing this erosion experimentally, many past efforts have focused on numerical modeling to predict erosion rates and thruster lifespan, but those analyses were limited to Hall thrusters operating in the 200–400...

متن کامل

A Compact Low-Power High-Isp Thruster for Microsatellites

Busek Co. Inc. completed delivery of flight-qualified colloid thrusters for NASA’s ST7 mission in May 2008. This effort has led to development of variants of the technology suitable for small satellite applications. Colloid thrusters operate by electrostatically accelerating charged droplets of an electrically conductive ionic liquid, and are capable of providing a high degree of throttling and...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2008