A Spacecraft for Ion Thrustor Flight Tests

640232

01/01/1964

Event
SAE World Congress & Exhibition
Authors Abstract
Content
A spacecraft that will be used for flight tests of ion thrustors is described. The spacecraft has been designed to provide measurements of thrustor electrical parameters and thrust. The tests to be carried out will determine the validity of ion thrustor performance data which have been obtained in vacuum chambers. The spacecraft, to carry two thrustors of different construction, will be launched into a ballistic trajectory by the NASA Scout vehicle. The test time will be approximately one hour.
Meta TagsDetails
DOI
https://doi.org/10.4271/640232
Pages
7
Citation
Gold, H., "A Spacecraft for Ion Thrustor Flight Tests," SAE Technical Paper 640232, 1964, https://doi.org/10.4271/640232.
Additional Details
Publisher
Published
Jan 1, 1964
Product Code
640232
Content Type
Technical Paper
Language
English