12-15 July 2011
Saint George Hotel
Africa/Johannesburg timezone

Miniaturization of electrostatic space thrusters using ionization/acceleration coupling in discharge mode

13 Jul 2011, 14:45
15m
Acro3

Acro3

Oral Presentation Track F - Applied and Industrial Physics Applied

Speaker

Dr phil ferrer (wits)

Description

Miniaturization of space prolusion systems has many advantages, both from an economic and performance perspective. One of the most promising propulsion technologies, the gridded electrostatic ion engine, resists miniaturization due to the poor down-scaling characteristics of the ion producing discharge chamber. We investigate a system where the ionization and acceleration mechanisms are coupled, thereby making the same electric field responsible for both. This sidesteps the need of a discharge chamber and allows for design of a much smaller engine. We introduce the concept and present some initial results, commenting on the feasibility of such a design.

Would you like to <br> submit a short paper <br> for the Conference <br> Proceedings (Yes / No)? yes
Level (Hons, MSc, <br> &nbsp; PhD, other)? other
Consider for a student <br> &nbsp; award (Yes / No)? no

Primary author

Dr phil ferrer (wits)

Presentation Materials