Optimization and calibration of thrust stand for micro-pulsed plasma thruster

A micro-pulsed plasma thruster is a plasma jet engine used in micro-satellite and nano-satellite to provide attitude control and changes in orbital height. The micro-pulsed plasma thruster will produce impulse bits to achieve its mission. Therefore, it is necessary to accurately measure the impulse...

Full description

Saved in:
Bibliographic Details
Main Author: Tan, Zhen Yong
Other Authors: Low Kay Soon
Format: Final Year Project
Language:English
Published: 2014
Subjects:
Online Access:http://hdl.handle.net/10356/60212
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Nanyang Technological University
Language: English