Electric Propulsion of Spacecraft
D. G. Fearn
Abstract
D. G. Fearn
Abstract
The Report commences with a discussion of the merits of electric propulsion technology, explaining that the very high exhaust velocities attainable allow the propellant masses required for most missions to be drastically reduced. The various types of electric thruster are then described briefly. The most highly developed and potentially useful thruster, the Kaufman electron bombardment ion thruster, is covered in greater detail, with particular reference to the T5 device developed in the UK. Candidate missions are discussed, ranging from attitude and orbit control functions to the application of ion propulsion to the deployment of solar power satellites. Important terrestrial applications of electric propulsion technology are also mentioned. (Author)
OpenAlex reports 12 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
The Report commences with a discussion of the merits of electric propulsion technology, explaining that the very high exhaust velocities attainable allow the propellant masses required for most missions to be drastically reduced. The various types of electric thruster are then described briefly. The most highly developed and potentially useful thruster, the Kaufman electron bombardment ion thruster, is covered in greater detail, with particular reference to the T5 device developed in the UK. Candidate missions are discussed, ranging from attitude and orbit control functions to the application of ion propulsion to the deployment of solar power satellites. Important terrestrial applications of electric propulsion technology are also mentioned. (Author)
Key concepts: Ion thruster, Electrically powered spacecraft propulsion, Propulsion, Aerospace engineering, Spacecraft, Propellant, Spacecraft propulsion, In-space propulsion technologies