Accession Number:

ADA461390

Title:

Vacuum Chamber Construction and Contamination Study of A Micro Pulsed Plasma Thruster

Descriptive Note:

Master's thesis

Corporate Author:

AIR FORCE INST OF TECHNOLOGY WRIGHT-PATTERSON AFB OH GRADUATE SCHOOL OF ENGINEERING AND MANAGEMENT

Personal Author(s):

Report Date:

2006-12-01

Pagination or Media Count:

127.0

Abstract:

The micro pulsed plasma thruster micro-PPT is a simple and versatile electric thruster capable of performing multiple missions, from precise attitude control on standard satellites to primary propulsion for nanosatellites. In order to fill this role as both industry and government move toward utilizing smaller satellites, micro-PPTs first need to be thoroughly tested on the ground. This study examines the deposition profile and rate of particle emission from the thruster so that satellite designers understand any potential contamination issues with sensitive instruments and solar panels. Employing a newly assembled vacuum chamber system, four tests were completed with the micro-PPTs, and the results showed that particles discharge in all directions, with the surfaces directly facing the propellant tube collecting exponentially more particle deposition than surfaces at wider angles.

Subject Categories:

  • Mechanics
  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE