{"id":39191,"date":"2015-11-23T20:46:43","date_gmt":"2015-11-23T12:46:43","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/nasa-awards-contracts-for-deep-space-advanced-propulsion-systems\/"},"modified":"2015-11-23T20:46:43","modified_gmt":"2015-11-23T12:46:43","slug":"nasa-awards-contracts-for-deep-space-advanced-propulsion-systems","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/nasa-awards-contracts-for-deep-space-advanced-propulsion-systems\/","title":{"rendered":"NASA awards contracts for deep-space advanced propulsion systems"},"content":{"rendered":"<p>NASA has awarded contracts to three American propulsion companies to aid the U.S. federal space agency with the development of advanced deep-space Electric Propulsion systems \u2013 including VASIMR \u2013 needed to one day transport astronauts to destinations beyond Low Earth Orbit (LEO).<\/p>\n<\/p>\n<p>\nNew Propulsion elements for deep-space exploration:<\/p>\n<p>As part of NASA\u2019s phased approach to the development of technology and systems needed to carry astronauts on long-duration, deep-space missions, the agency\u2019s Human Exploration Operations Mission Directorate\u2019s (HEOMD\u2019s) Advanced Exploration Systems (AES) division has committed to the \u201crapid development and testing of prototype systems and validation of operational concepts to reduce risk and cost of future exploration missions.\u201d<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" class=\"alignleft\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/09\/2015-09-24-220056-350x215.jpg\" alt=\"2015-09-24-220056\" width=\"350\" height=\"215\">Part of this initiative includes the development of systems that will aid in the human and robotic exploration of Beyond Earth Orbit targets.<\/p>\n<p>To do so, however, requires new propulsion systems that have previously been unnecessary for Near Earth Orbit exploration \u2013 where traditional chemical-based propulsion works best toward the short duration and relative close proximity of missions and their destinations.<\/p>\n<p>To support the development of these new systems, a set of three objectives for in-space power and propulsion were developed.<\/p>\n<p>According to the HEOMD\u2019s AES status update from 4 November 2015, these objectives include the development of a 100 kW&nbsp;class Solar Electric Propulsion (SEP) system, as well as the development of technologies for \u201cnuclear thermal propulsion to enable rapid transport of crew to Mars\u201d and development of \u201chigh energy, modular power systems for exploration missions.\u201d<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>SLS\/BEO Forum Section<\/li>\n<li>     (adsbygoogle = window.adsbygoogle <\/li>\n<li>Advanced Forum Section<\/li>\n<li>L2 SLS\/BEO Section<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>To accomplish these objectives, NASA has contracted with three commercial companies&nbsp;to undertake a 100 continuous hour test of&nbsp;100 kW&nbsp;electric propulsion systems<\/p>\n<p>Additionally, progress is also being made on the development of \u201cfuel elements, reactor concepts, and affordable ground testing methods\u201d for nuclear thermal propulsion design.<\/p>\n<p>To date, in addition to the contract awards already in place, NASA and its partner&nbsp;agencies have completed fabrication and testing of a new graphite composite fuel element for a 2,800K hot hydrogen flow system for potential nuclear thermal propulsion elements.<\/p>\n<p>Contracts and specific goals:<\/p>\n<p>To accomplish all of the advanced propulsion goals, NASA awarded three contracts to Ad Astra, MSNW, and Aerojet Rocketdyne to develop \u201cpropulsion technology systems in the 50- to 300-kW range to meet the needs of a variety of deep-space mission concepts beyond capabilities currently being developed for ARM (Asteroid Return Mission) SEP,\u201d notes the HEOMD AES presentation.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-42640\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125905-350x266.jpg\" alt=\"2015-11-23-125905\" width=\"350\" height=\"266\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125905-350x266.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125905.jpg 453w\" sizes=\"(max-width: 350px) 100vw, 350px\">In all, the three private companies&nbsp;were chosen by NASA to develop \u2013 via fix-priced, milestone&nbsp;achievement contracts \u2013 an advanced electric propulsion (EP) system over a three year period.<\/p>\n<p>These developed EP&nbsp;systems must have a broad specific impulse range of 2,000 to 5,000 seconds, an operational end-to-end total efficiency greater than 60%, and an in-space lifetime greater than 50,000 hours (with more than 10,000 of those hours specifically designed for operational use).<\/p>\n<p>Moreover, the systems must have a total mass less than 5kg\/kW.<\/p>\n<p>In the&nbsp;final year of the contracts, all three companies are expected to be able to demonstrate an EP system with a \u201cminimum of 100 hours of continuous operations at power levels of at least 100 kWs in a relevant TRL 5 (NASA Technology Readiness Level 5) environment.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-42634\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125120-350x199.jpg\" alt=\"2015-11-23-125120\" width=\"350\" height=\"199\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125120-350x199.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125120.jpg 471w\" sizes=\"(max-width: 350px) 100vw, 350px\">To this end, Ad Astra has agreed to develop a Thermal Steady State VASIMR (VAriable Specific Impulse Magnetoplasma Rocket) with \u201cscaleability for human spaceflight.\u201d<\/p>\n<p>VASIMR propulsion technology uses radio waves to ionize and heat propellant and magnetic fields that in turn create a plasma that is then accelerated to create thrust for a spacecraft.<\/p>\n<p>VASIMR\u2019s method of heating plasma for&nbsp;propulsion purposes was first developed from research surrounding nuclear fusion.<\/p>\n<p>For Ad Astra, NASA awarded the Texas-based company a contract on 7 August 2015 \u2013 which will be in effect through 6 August 2018 with two, one year options.<\/p>\n<p>Already, Ad Astra has revealed that it plans to complete all subsystems for their VASIMR test article by August 2016.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-42639\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125706-350x196.jpg\" alt=\"2015-11-23-125706\" width=\"350\" height=\"196\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125706-350x196.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125706.jpg 481w\" sizes=\"(max-width: 350px) 100vw, 350px\">This process will take Ad Astra through the first year of its system design, which will then continue&nbsp;into the second year of operations and testing when the company will perform first and second stage low thrust plasma tests.<\/p>\n<p>The second year of the contract will also see Ad Astra complete second stage and plasma dump preparations as well as conduct first and second stage integrated low thrust plasma tests.<\/p>\n<p>All of this work will lead to the third year of the contract, when an integrated duration high thrust plasma test is slated to occur.<\/p>\n<p>Throughout Ad Astra\u2019s three-year contract, the company will demonstrate a \u201c5 single core VASIMR thruster with PPUs (Power Processing Units), the VX-200SS, in thermal steady-state for at least 100 continuous hours at 100 kW.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-42638\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125557-350x279.jpg\" alt=\"2015-11-23-125557\" width=\"350\" height=\"279\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125557-350x279.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125557-439x350.jpg 439w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125557.jpg 575w\" sizes=\"(max-width: 350px) 100vw, 350px\">The contract from NASA, worth $9.06 million USD, will allow Ad Astra to \u201cLeverage its privately funded superconducting magnet, propellant management system, power processing units, and unique vacuum capabilities to test the steady-state performance of its integrated thermal design.\u201d<\/p>\n<p>In addition to the $9.06 million USD contract from NASA, Ad Astra will also share approximately $11.78 million USD as part of the development process.<\/p>\n<p>However, it is not just the Ad Astra company that NASA has turned to for development of new EP technologies.<\/p>\n<p>The Washington state based Limited Liability Company MSNW won a contract from NASA on 17 September 2015 for development of a flexible high power electric propulsion system for exploration class missions, notes the HEOMD AES presentation.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-42635\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125219-350x200.jpg\" alt=\"2015-11-23-125219\" width=\"350\" height=\"200\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125219-350x200.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125219.jpg 455w\" sizes=\"(max-width: 350px) 100vw, 350px\">MSNW\u2019s contract from NASA is worth $1.5 million USD, with a total cost sharing of $1.5 million USD, for development of a 100 Joule electrodeless Lorentz Force thruster.<\/p>\n<p>MSNW, whose contract will last until 16 September 2018, has a 36 month schedule which will see the first 6 months focused on thruster assembly.<\/p>\n<p>By the 12th month of the contract, MSNW will have a full thermal engineering model of a 100 kW pulse operated thruster.<\/p>\n<p>Two years into the contract, the company will have demonstrated \u201csteady thermo-vac thruster and PPU operations.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/09\/2015-09-24-220509-350x252.jpg\" alt=\"2015-09-24-220509\" width=\"350\" height=\"252\">Three months later, MSNW will have completed upgrades to its Pulsed High power facility, all leading to a 100 hour, 100-200 kW integrated test in the 36th month of the contract.<\/p>\n<p>Moreover, in addition to Ad Astra and MSNW, NASA is also understood to be in contract negotiations with the Aerojet Rocketdyne company, also based in Washington state, for development of a 100 kW EP system with a 250 kW nested Hall thruster.<\/p>\n<p>As of publication of the HEOMD AES presentation on 4 November 2015, the contract between NASA and Aerojet Rocketdyne had not yet been finalized, though the presentation does note that the contract award is expected in late November.<\/p>\n<p>This contract, however, differs from the others as it is a 12-month base contract with two one-year options.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-42637\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125428-350x264.jpg\" alt=\"2015-11-23-125428\" width=\"350\" height=\"264\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125428-350x264.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125428-464x350.jpg 464w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-23-125428.jpg 506w\" sizes=\"(max-width: 350px) 100vw, 350px\">Aerojet Rocketdyne\u2019s contract will see the company \u201cDemonstrate performance capabilities to TRL 5 with 100 kW input power for 100 hour at thermal steady-state, implement the XR-250, 250 kW Hall thruster, and demonstrate the XR-100, 100 kW system extensible to MW class systems.\u201d<\/p>\n<p>Despite the difference in contracts, Aerojet Rocketdyne has developed a three-year test program, in which the first year will see the testing and demonstration of components for the system, a second year demonstration and test in the TRL 4 category, followed by a third-year demonstration test in the TRL 5 category.<\/p>\n<p>The total contract from NASA is understood to be worth $6.273 million USD, with government directed funding to GRC of $986,000 and to JPL of $722,000.<\/p>\n<p>An additional $11.958 million USD will be contributed through Team Corporate, though all of these figures are subject to final negotiations.<\/p>\n<p>(Images:&nbsp;Via NASA and L2)<\/p>\n<p>(To join L2, click here:&nbsp;http:\/\/www.nasaspaceflight.com\/l2\/)<\/p>\n","protected":false},"excerpt":{"rendered":"<p>NASA has awarded contracts to three American propulsion companies to aid the U.S. federal space agency with the development of advanced deep-space Electric Propulsion systems \u2013 including VASIMR \u2013 needed to one day transport astronauts to destinations beyond Low Earth Orbit (LEO). New Propulsion elements for deep-space exploration: As part of NASA\u2019s phased approach to [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":30231,"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":[9007,9025],"class_list":["post-39191","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-news","tag-beo","tag-sep"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39191"}],"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=39191"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39191\/revisions"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media\/30231"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=39191"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=39191"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=39191"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}