Published February 1983 | Version v1
Report Restricted

Sputtering phenomena in ion thrusters. Final Report

Description

Sputtering effects in discharge chambers of ion thrusters are lifetime limiting in basically two ways: (1) ion bombardment of critical thruster components at energies sufficient to cause sputtering removes significant quantities of material enough to degrade operation through adverse dimensional changes or possibly lead to complete component failure, and (2) metals sputtered from these intensely bombarded components are deposited in other locations as thin films and subsequently flake or peel off the flakes then lodge elsewhere in the discharge chamber with the possibility of providing conductive paths for short circuiting of thruster components such as the ion optics. This experimental work has concentrated in two areas. The first has been to operate thrusters for multi-hour periods and to observe and measure the films found inside the thruster. The second was to simulate the environment inside the discharge chamber of the thruster by means of a dual ion beam system. Here, films were sputter deposited in the presence of a second low energy bombarding beam to simulate film deposition on thruster interior surfaces that undergo simultaneous sputtering and deposition. Mo presents serious problems for use in a thruster as far as film deposition is concerned. Mo films were found to be in high stress, making them more likely to peel and flake

Availability note (English)

MF available from INIS under the Report Number; Available from NTIS, PC A03/MF A01.

Files

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Additional details

Publishing Information

Imprint Pagination
32 p.
Report number
N--8418322

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
16003923
Subject category
S74: ATOMIC AND MOLECULAR PHYSICS;
Descriptors DEI
CURRENT DENSITY; FARADAY EFFECT; MOLYBDENUM; SPUTTERING; STRESSES; TANTALUM; THIN FILMS; TITANIUM
Descriptors DEC
ELEMENTS; FILMS; METALS; TRANSITION ELEMENTS

Optional Information

Secondary number(s)
NASA-CR--168172.