A Propulsion Device for Spacecraft

2005-01-3374

10/03/2005

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
A method that exploits certain properties of a recirculating gas has been investigated as a means of achieving a sustained accelerative vector force without either the expulsion of mass from or a reaction against an external mass by the accelerated body. A theory of operation is presented that defines the capabilities and limitations of the method, and which has resulted in functioning prototypes. The prototype devices require only a source of electric power and a means of cooling to achieve an internally generated, externally measurable accelerative vector force that is sustained for as long as power is supplied to the device.
Meta TagsDetails
DOI
https://doi.org/10.4271/2005-01-3374
Pages
11
Citation
Brady, J., "A Propulsion Device for Spacecraft," SAE Technical Paper 2005-01-3374, 2005, https://doi.org/10.4271/2005-01-3374.
Additional Details
Publisher
Published
Oct 3, 2005
Product Code
2005-01-3374
Content Type
Technical Paper
Language
English