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<\/p>\nConstruction of the living and working area for the first crewed Orion spacecraft is well underway at the Michoud Assembly Facility (MAF) in New Orleans. Building on lessons learned from previous construction, Orion prime contractor Lockheed Martin has already completed four of the seven welds necessary to assemble the crew module pressure vessel.<\/p>\n
Current schedules call for the completed pressure vessel to be shipped in September to the Kennedy Space Center (KSC) in Florida, where it will be outfitted to fly on Exploration Mission-2 (EM-2).<\/p>\n
\u201cWe\u2019ve done the PV1 weld \u2014 that\u2019s the tunnel to the forward bulkhead \u2014 [and] we just completed the three cone welds,\u201d Blaine Brown, Orion Crew Module Engineering Manager for Lockheed Martin, said in an interview with NASASpaceflight.com. \u201c[The] next one that we\u2019ll do is the aft bulkhead to the barrel.\u201d<\/p>\n
At the time of the interview on February 7, Brown also noted that the aft bulkhead was the last piece to arrive at MAF: \u201cThe bulkhead is in the process of being transported to Michoud today, actually, and the barrel is already at Michoud.\u201d<\/p>\n
The crew module pressure vessel consists of seven major welded components: a tunnel, three cone panels, a barrel, and two bulkheads. AMRO Fabricating Corporation in South El Monte, California, manufactures the three cone panels and Ingersoll Machine Tools in Rockford, Illinois, manufactures the other four components.<\/p>\n
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Orion welding, via NASA.<\/p>\n
EM-2 will be the first Orion mission to fly with crew, with its mission currently scheduled for no earlier than 2023.<\/p>\n
\u201cIt\u2019s really historical, not just from a technology standpoint,\u201d Paul Anderson, director of Orion EM-2 production at Lockheed Martin said. \u201cIt is the future vehicle of NASA to do space exploration, but this specific EM-2 mission will take humans further than any time in history.\u201d The EM-2 mission is currently planned to be a circumlunar flight.<\/p>\n
The pressure vessel is the structural core of the crew module. Other elements such as systems for thermal protection (the heatshield), propulsion (attitude control), and landing and recovery (parachutes and flotation) attach to the outside of the pressure vessel, in addition to other primary and secondary structures.<\/p>\n
It is also the crew cabin \u2014 the living and working area for the astronauts on the mission. Most of the time, a sea-level atmosphere in the pressure vessel will be maintained for the crew. Inside the pressure vessel are areas for crew systems such as flight controls, communication and information systems, seating, storage for food, clothes, and equipment, a galley, and a toilet.<\/p>\n
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Welding taking place at MAF \u2013 via NASA.<\/p>\n
The pressure vessel is welded together in a sequence of welds. With the tunnel joined to the inside of the forward bulkhead and the cone formed by those three panels, those two sub-assemblies will be welded by joining the outside of the forward bulkhead to the top of the cone. Separately, the bottom of the barrel will also be welded to the aft bulkhead.<\/p>\n
Once those welds are complete, the pieces will almost be ready for the final weld. \u201cThe final weld is the closeout weld, where we weld the cone to the barrel,\u201d Brown said.<\/p>\n
Before that final weld, the other major structural component has to be added to the aft bulkhead, called the backbone assembly. \u201cIt\u2019s a structural reinforcement, as well as providing basically areas where we can then put the crew equipment, stowage, all that kind of stuff,\u201d he explained.<\/p>\n
\u201cWe\u2019ve got running crossbeams through there, and it also serves as a partition. That\u2019s where our lockers go and it\u2019s also where you\u2019ve got the area where the toilet is and also the galley for the crew.\u201d<\/p>\n
The backbone assembly is a bolted structure consisting of nine pieces that are assembled prior to being installed inside the pressure vessel. \u201cWe actually have a very nice tool that we can build that whole backbone up, separately, get it all in alignment, get it all precise, and then it fits right into the barrel\/aft bulkhead area,\u201d Brown noted.<\/p>\n
The backbone is also bolted into the welded aft bulkhead\/barrel assembly.<\/p>\n
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Backbone of Orion (background) near the CM. Photo by Philip Sloss for NSF.<\/p>\n
The EM-2 pressure vessel is the fifth structure to be constructed at MAF. The first two Ground Test Article (GTA) and Exploration Flight Test-1 (EFT-1) structures were pathfinders for the program in terms of production, processing and handling, and flight.<\/p>\n
Taking the lessons learned from the GTA structure and EFT-1 vehicle, the pressure vessel was improved to reduce the number of parts and overall weight while maintaining its required strength. From the GTA pressure vessel (the first) to the EM-1 pressure vessel (the third), the design reduced the number of components from thirty-one pieces to seven and reduced the overall weight from 3900 pounds to 2700.<\/p>\n
The lessons learned have also led to improvements being fed back into manufacturing, assembly, and production.<\/p>\n
\u201cWe\u2019ve really been through this multiple times already,\u201d Brown noted. \u201cThe EM-1 and structural test article (STA) [pressure vessels] have been basically following the same process, so we\u2019ve really wrung this [process] out and applied lessons learned in doing this.\u201d<\/p>\n
\u201cIt had taken three weeks to a month to get through these welds like on the cone [panels],\u201d he explained. \u201cOriginally even longer, because we were [new to] getting the alignments [correct] and here it was like a week and a half to get through the three of them. As you would expect, you learn on each of the builds and we\u2019ve done it many times now.\u201d<\/p>\n
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Orion production flow at MAF \u2013 via NASA.<\/p>\n
\u201cThe entire MAF operation [has] gone extraordinarily well,\u201d Anderson added. \u201cWhether it was on the STA, EFT-1, [or] EM-1, every time we do this we apply whatever lessons learned to tooling, whether it\u2019s tolerances to manufacturing. All of this we have started to see pay dividends.\u201d<\/p>\n
\u201cWe have really seen improvements [in] how well these things have gone together,\u201d Anderson continued. \u201cThe supplier performance of the seven major elements, whether it was Ingersoll or AMRO, has been I would say significantly better. Just because they\u2019ve learned as well, there are all these similar operations within their factories.\u201d<\/p>\n
\u201cAnd we\u2019re really excited about that as we head into the production phase of this contract that will hopefully be started later this year. So we\u2019re really starting to see efficiencies, time reductions, and cost reductions, and it\u2019s really exciting to see.\u201d<\/p>\n
Each of the pressure vessel welds has its own tool where the parts are welded. \u201cThere is specialized tooling for each one of these [welds] that we custom fabricate,\u201d Brown explained.<\/p>\n
\u201cThe actual weld head itself [is] basically the same, but we have different tooling to basically line up each of the different parts to get the weld interfaces in exactly the right alignment and hold them into place while we go do the weld sequence.\u201d Self-reacting friction stir welding is used for each of the welds.<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/02\/2018-02-14-144231.jpg\")
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Welding tool for Orion \u2013 via NASA.<\/p>\n
After welding, non-destructive evaluation (NDE) is used to inspect them. \u201c[We use] ultrasonic inspections there to basically look for any kind of defects or flaws that are in those,\u201d he said.<\/p>\n
Brown also explained another work item for some of the welds: \u201cWe do what we call \u2018planishing.\u2019 [That] is where you literally pound it with a hammer,\u201d he explained.<\/p>\n
\u201cThat\u2019s basically stress relief on those particular welds. We\u2019ve worked with that quite a bit in the past to identify which are the critical welds that we need to [remove] any kind of residual stresses that come from the weld process and the fit-up process itself.\u201d<\/p>\n
Once the pressure vessel is fully welded, bolted, and inspected, it will be cleaned and prepared to ship from MAF to KSC. \u201cThere\u2019s a shipping tool that we have, a fixture,\u201d Brown said. \u201cYou basically wrap it all up good and tight inside, and then you put it in this shipping crate.\u201d<\/p>\n
The pressure vessel can be shipped to KSC either by ground on a truck or by air using NASA\u2019s Super Guppy aircraft. \u201cWe\u2019ve done both ways, truck and Guppy,\u201d Brown added.<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/02\/2018-02-14-144440.jpg\")
<\/p>\n
EM-1 Orion on NASA\u2019s Super Guppy \u2013 via NASA.<\/p>\n
\u201c[If] it goes on the truck, it\u2019s then a wide load and we have a certain route, we do permits and all that kind of stuff to get it from Michoud over to KSC. Certainly, the Guppy is the quickest [but] it depends on urgency and availability of the Guppy. The Guppy is the easiest one, but sometimes it\u2019s not necessarily available when we need it.\u201d<\/p>\n
Anderson said the pressure vessel is currently scheduled to arrive in Florida in September. Once it arrives there and is transported to the Orion spacecraft processing area in the Operations and Checkout (O&C) Building at KSC, work will begin to complete the overall structure of the crew module.<\/p>\n
\u201cWe do what we call birdcage operations,\u201d Anderson explained. \u201cThe birdcage is literally a tool down at the O&C that houses the primary structure. It enables us to install other elements of what we\u2019re calling the primary structure [that are] not pressure vessel related. We do secondary structure installation that\u2019s about the first five or six months, [where] we finish out what we\u2019re calling [the primary structure].\u201d<\/p>\n
One of the early processing milestones at KSC is proof pressure testing, which verifies that the pressure vessel is air-tight. The structure is sealed and pressurized above and beyond the maximum expected pressure; this verifies structural integrity and margin.<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/02\/2018-02-14-144548.jpg\")
<\/p>\n
EM-1 Orion at KSC \u2013 via NASA<\/p>\n
\u201cWe won\u2019t have the final flight hatch configuration at that point, but basically we have [verified the] integrity of the pressure vessel,\u201d Anderson added. \u201cWe\u2019ll instrument that and so on in that proof pressure test.\u201d<\/p>\n
Farther into processing, the spacecraft will continue to follow in the EM-1 crew module\u2019s footsteps.<\/p>\n
\u201cWe\u2019ll begin to install propulsion, we\u2019ll begin to install harnesses, some of the ECLSS (Environmental Control and Life Support System) components, as we build up,\u201d Anderson noted.<\/p>\n
\u201cWe\u2019ll do welding for propulsion and ECLSS \u2014 that\u2019s going to be our clean room operation. Within the O&C, there\u2019s both clean room ops and normal ops. When we do welding we have to go to the clean room.\u201d<\/p>\n","protected":false},"excerpt":{"rendered":"
Construction of the living and working area for the first crewed Orion spacecraft is well underway at the Michoud Assembly Facility (MAF) in New Orleans. Building on lessons learned from previous construction, Orion prime contractor Lockheed Martin has already completed four of the seven welds necessary to assemble the crew module pressure vessel. Current schedules call […]<\/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":[4011,7866,640],"class_list":["post-38547","post","type-post","status-publish","format-standard","hentry","category-news","tag-em-2","tag-maf","tag-orion"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/38547"}],"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=38547"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/38547\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=38547"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=38547"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=38547"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}