Abstract
This paper presents the development of an electrostatic calibration system that produces consistent and reproducible calibration force over three orders of magnitude in the range 30 μN-3.4 mN with a deviation error of less than 2%. In the proposed approach, the electrostatic force is generated using a pair of heat sinks that is electrically charged with high voltage and engaged at a particular distance. Precise control of the high-voltage pulses applied to the calibrator produces calibration impulse bit in the range 7-340 μNs. The calibrator is used to tune a torsional thrust stand that performs measurements of constant and impulsive force from any micropropulsion system.
| Original language | English |
|---|---|
| Pages (from-to) | 3467-3475 |
| Number of pages | 9 |
| Journal | IEEE Transactions on Instrumentation and Measurement |
| Volume | 64 |
| Issue number | 12 |
| DOIs | |
| Publication status | Published - Dec 2015 |
Keywords
- Electrostatic
- micronewton
- satellite micropropulsion
- thrust stand
ASJC Scopus subject areas
- Instrumentation
- Electrical and Electronic Engineering