Engineering Papers⌕ Search

NASA NTRS · 20060051529

VHITAL-160 Thruster Development Status

Abstract

A general overview on the status of the Very High Isp Thruster with Anode Layer (VHITAL)-160 program is presented. The topics include: 1) Bi TAL Overview; 2) VHITAL Program Overview; 3) Thruster Fabrication; and 4) Thruster Testing.

Explore related subjects

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Sengupta, Anita, Marrese-Reading, Colleen, Hofer, Rich, Owens, Al, Swindlehurst, Ray, Fitzgerald, Dennis. 2006-01-01. VHITAL-160 Thruster Development Status. https://ntrs.nasa.gov/citations/20060051529

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

Non-Intrusive Characterization of the Wear of the HERMeS Thruster Using Optical Emission Spectroscopy

The Hall Effect Rocket with Magnetic Shielding (HERMeS) is a 12.5 kW Hall thrusterelectric propulsion string that has been in development by NASA Glenn Research Center(GRC) and NASA JPL since 2012. Due to the magnetically shielded design, service life-limiting erosion of the boron nitride discharge has been virtually eliminated. The innerfront pole cover (IFPC) has now been identied as the component dening erosion-basedservice life. Optical emission spectroscopy (OES) is used as an in-situ diagnostic to measurerelative erosion trends during operation of the HERMeS thruster during a series of shortduration wear tests. Erosion trends obtained from the OES data will be compared totraditional erosion data measured with a non-contact prolometer.

hall thruster↗