The European Space Agency (ESA) have successfully tested a new engine, called the Dual-Stage 4-Grid (DS4G) ion thruster, claimed to be a jump forward in the form of electric propulsion which accelerates a beam of positively charged particles (ions) as propulsion using an electric field. <\/p>\n
The new engine is ten times more fuel efficient than their current form of electric propulsion, as used on ESA\u2019s Moon probe SMART-1.\n<\/p>\n
In cooperation with the Australian National University, ESA believe the DS4G marks a major step forward in space propulsion capability, based around a concept designed by David Fearn, a pioneer of ion propulsion in the UK.<\/p>\n \u2018Using a similar amount of propellant as SMART-1, with the right power supply, a future spacecraft using our new engine design wouldn\u00e2\u20ac\u2122t just reach the Moon, it would be able to leave the Solar System entirely,\u2019 said Dr Roger Walker of ESA\u00e2\u20ac\u2122s Advanced Concepts Team, Research Fellow in Advanced Propulsion and Technical Manager of the project. <\/font><\/p>\n Previous ion engines use three closely separated perforated grids containing thousands of millimetre-sized holes attached to a chamber containing a reservoir of the charged particles. The first grid has thousands of volts applied, and the second grid operates at low voltage. The voltage difference over the gap between the two grids creates an electric field that acts to simultaneously extract and accelerate the ions out of the chamber and into space in a single step. <\/p>\n The higher the voltage difference, the faster the ions are expelled and the greater the fuel efficiency of the thruster. However, at higher voltage differences approaching five thousand volts (5kV), some of the ions collide with the second grid as they are accelerated, thus eroding and damaging the grid and thereby limiting its lifetime in space. <\/font><\/p>\n The DS4G ion engine utilises a different concept first proposed in 2001 by Fearn, which solves this limitation by performing a two-stage process to decouple the extraction and acceleration of ions using four grids. In the first stage, the first two grids are closely spaced and both are operated at very high voltage and a low voltage difference between the two (3 kV) enables the ions to be safely extracted from the chamber without hitting the grids. <\/p>\n Then, in the second stage, two more grids are positioned at a greater distance \u00e2\u20ac\u02dcdownstream\u00e2\u20ac\u2122 and operated at low voltages. The high voltage difference between the two pairs of grids powerfully accelerates the extracted ions. <\/font><\/p>\n The test model achieved voltage differences as high as 30kV and produced an ion exhaust plume that travelled at 210,000 m\/s, over four times faster than state-of-the-art ion engine designs achieve. <\/p>\n This makes it four times more fuel efficient, and also enables an engine design which is many times more compact than present thrusters, allowing the design to be scaled up in size to operate at high power and thrust. Due to the very high acceleration, the ion exhaust plume was very narrow, diverging by only 3 degrees, which is five times narrower than present systems. This reduces the fuel needed to correct the orientation of spacecraft from small uncertainties in the thrust direction. <\/font><\/p>\n \u00e2\u20ac\u0153Working with our industrial partners, the next challenge is to transition this promising new engine design from laboratory experiment to spacecraft flight model and properly define the new missions that it will enable\u00e2\u20ac\u009d, says Jos\u00c3\u00a9 Gonzalez del Amo, Head of Electric Propulsion at ESA. The flight-suitable engines must then be tested: and for ion engines this is a long process. <\/font><\/p>\n Since they must operate continuously in space for tens of thousands of hours providing a small thrust, ground tests in a vacuum facility must last several thousand hours to prove their reliability. Only after all this could the first flight models be launched. <\/font><\/p>\n Space Technology (adsbygoogle = window.adsbygoogle || []).push({});<\/p>\n Once ready, these engines will be able to propel spacecraft to the outermost planets, the newly discovered planetoids beyond Pluto and even further, into the unknown realm of interstellar space beyond the Solar System. Closer to home, these supercharged ion engines could figure prominently in the human exploration of space. With an adequate supply of electrical power, a small cluster of larger, high power versions of the new engine design would provide enough thrust to propel a crewed spacecraft to Mars and back. <\/font><\/p>\n \u2018This is an ultra-ion engine. It has exceeded the current crop by many times and opens up a whole new frontier of exploration possibilities,\u2019 added Dr Walker.<\/p>\n Related forum thread: Specific ESA forum section: The European Space Agency (ESA) have successfully tested a new engine, called the Dual-Stage 4-Grid (DS4G) ion thruster, claimed to be a jump forward in the form of electric propulsion which accelerates a beam of positively charged particles (ions) as propulsion using an electric field. The new engine is ten times more fuel efficient than […]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[],"class_list":["post-42183","post","type-post","status-publish","format-standard","hentry","category-news"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/42183"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=42183"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/42183\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=42183"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=42183"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=42183"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}
<\/em><\/font>http:\/\/forum.nasaspaceflight.com\/forums\/thread-view.asp?tid=1240&start=1<\/em><\/font><\/p>\n
<\/em><\/font>http:\/\/forum.nasaspaceflight.com\/forums\/forum-view.asp?fid=17<\/em><\/font><\/p>\n","protected":false},"excerpt":{"rendered":"