[HN Gopher] Workmanship standard for crimping, interconnecting c...
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       Workmanship standard for crimping, interconnecting cables,
       harnesses, and wiring
        
       Author : throw0101c
       Score  : 98 points
       Date   : 2024-06-02 16:53 UTC (6 hours ago)
        
 (HTM) web link (standards.nasa.gov)
 (TXT) w3m dump (standards.nasa.gov)
        
       | OldGuyInTheClub wrote:
       | Before I worked in aerospace, I wondered why that industry cost
       | so much. Now I understand that every requirement within each
       | requirement document has to be "flowed down," maintained,
       | verified, documented, and that compliance has to be proven along
       | the chain from design to operation. The number of these documents
       | grows at some beyond-linear rate with project complexity.
       | 
       | Of course, this is not all the source of cost but it is a good
       | chunk. But, if you're building spaceflight hardware that can't be
       | repaired once launched, it is necessary.
        
         | mschuster91 wrote:
         | ... and all of the documentation has to be kept around _for
         | decades_ , same for the knowledge of how it was constructed and
         | maintained. That's what makes missions like Voyager or even the
         | ISS _possible_ in the first place - a lot of the people who did
         | the early work on either are probably dead now.
        
         | tekla wrote:
         | When I worked on some aircraft, every single line of code that
         | was added or changed had a digital and paper record of the
         | change and the reason for it.
        
         | neilv wrote:
         | Inspired by very serious traceability, like for aerospace
         | engineering, I did a very-very simple and lightweight system,
         | for the security practices & assurances of a non-aerospace
         | startup.
         | 
         | I was proud of not only of how effective yet non-encumbering
         | the practices, and how smart our external assurances, but the
         | lightweight way of implementing traceability between the two. A
         | single, short _internal_ document tracked not only practices,
         | but sections were annotated with all the _external_ documents
         | /instances that made assurances wrt to those practices. So when
         | we did need to change something, we knew what was easy and hard
         | to change. (Interface vs. implementation.)
         | 
         | Of course, the very first externally-shareable document side of
         | this, I explained to our enterprise salesperson that it would
         | convince the partner's savvy IT people that we were fully
         | competent and diligent, and said a bit about how everything in
         | there was carefully designed and traceable... Well, maybe you
         | can guess how that went.
         | 
         | Not everyone is familiar with building things that really have
         | to work correctly, nor with how a little bit of judicious
         | process can actually make things dramatically more efficient,
         | nor with any kind of traceability rigor. If you're not familiar
         | with that, or aren't aligned with that, then the most efficient
         | thing in your mind might be to quietly change a copy of
         | engineering document, to say whatever is most expedient in the
         | moment. And don't tell anyone that you changed a copy of an
         | engineering document, since that would not be a happy vibe when
         | everyone likes what you're saying, and so not a good use of
         | your time. :)
         | 
         | (I default to confidentiality about such things, even in
         | absence of NDA. But I can mention this anecdote, in this
         | professional practice discussion within the field, since the
         | company is no longer in business, and there are no unresolved
         | liabilities.)
        
           | newsclues wrote:
           | I think it may be seen as a feature not a bug when there is
           | cost plus contracts and regulatory capture limits
           | competition.
        
             | OldGuyInTheClub wrote:
             | I will agree that there is a lot of overhead per
             | engineering hour in this market area. But, I also think
             | there's a great deal of misunderstanding about how
             | government contracting works. Cost-plus fixed fee means the
             | fee is agreed upon at the outset. If you overrun you may
             | get the cost of the extra work performed but you get no fee
             | (profit) on it. When the corporation sees that dilution,
             | there is usually hell to pay. If the government gets tired
             | of the overruns, it can and does cancel the contract.
             | 
             | There are different contract types with award fee and/or
             | incentive fees each with its own peculiarities.
             | 
             | The Federal Acquisition Regulations (FAR) make for
             | interesting reading:
             | 
             | https://www.acquisition.gov/far/part-16
             | 
             | " Part 16 - Types of Contracts"
        
         | euroderf wrote:
         | Oh but we're bringing in some hotshots from McKinsey who have
         | some ideas about how we can trim all this unnecessary overhead.
         | They have assured me that absolutely nothing can go wrong.
        
       | nickt wrote:
       | There were some good comments last time around, I can't believe
       | that was 9 years ago!
       | 
       | https://news.ycombinator.com/item?id=9905875
        
       | Modified3019 wrote:
       | A personal favorite, the Fastener Design Manual:
       | https://ntrs.nasa.gov/citations/19900009424
       | 
       | In particular
       | 
       | >Lockwashers
       | 
       | >The typical helical spring washer shown in figure 14 is made of
       | slightly trapezoidal wire formed into a helix of one coil so that
       | the free height is approximately twice the thickness of the
       | washer cross section. They are usually made of hardened carbon
       | steel, but they are also available in aluminum, silicon, brome,
       | phosphor-bronze, stainless steel, and K-Monel. The lockwasher
       | serves as a spring while the bolt is being tightened. However,
       | the washer is normally flat by the time the bolt is fully
       | torqued. At this time it is equivalent to a solid flat washer,
       | and its locking ability is nonexistent. In summary, a lockwasher
       | of this type is useless for locking.
        
         | petee wrote:
         | Someone on YT did a demonstration on a paint shaker, and the
         | bolts loosen nearly as fast as having none. Internal/external
         | tooth washers or nylocks are the way to go
        
           | cuSetanta wrote:
           | Nordlock washers are the best, but they are expensive and a
           | little space inefficient.
        
         | analog31 wrote:
         | One useful property is that when partially tightened, they
         | allow slight re-positioning of an assembly, before driving the
         | fastener all the way home. In other words, they're actually
         | used as springs.
        
       | cuSetanta wrote:
       | As a spacecraft Assembly, Integration and Test (AIT) Engineer,
       | one of my areas of expertise is harness manufacture and routing.
       | So this naturally involves an awful lot of crimping. I am a
       | certified crimping operator and inspector under the ECSS
       | standards (which go a bit overboard at times in their
       | requirements when compared to the NASA standards).
       | 
       | I am lucky to have built a large amount of harness has/is/will
       | fly on many spacecraft for many customers. There are a lot of
       | unique challenges to crimping for spacecraft harnessing, but in
       | almost all circumstances the main issue has be schedule. Very few
       | project managers that I have worked with, even those who have a
       | lot of experience, plan for enough time to complete the
       | harnessing side of a project.
       | 
       | Depending on the number of crimping configurations that are
       | present in a system, it can take days to calibrate all of the
       | crimp tools before starting. Every crimp needs to be inspected
       | before the heatshrink can be shrunk, and often before the next
       | crimp can be performed if the routing is critical. Routing
       | involves labeling, gluing of tie-bases, bundling of harnessing,
       | and the shielding.... jesus christ the shielding can be a
       | nightmare...
       | 
       | Man I love making harness, honestly one of my favourite things to
       | make. Not sure if anyone cares enough to have questions, but
       | happy to answer them if they exist.
        
         | goy wrote:
         | I'd like to know more about the education & career path that
         | lead you there ...
        
           | cuSetanta wrote:
           | At undergraduate level I studied Physics and Astronomy, and
           | then did a research MSc as an optical astronomer, which I
           | hated and drove me away from Physics and Astronomy as a
           | whole.
           | 
           | I spent a few years working in IT Support before deciding to
           | go back to University to study Spacecraft Engineering at
           | Surrey University. Which was a wonderful course, that gave an
           | incredible overview of how one builds a spacecraft. More than
           | most of the Master programs I have seen in the field since,
           | the guys at Surrey had very real experience building quite a
           | few spacecraft, which shone through in the projects and
           | courses.
           | 
           | After that I started a PhD in Southampton that had an
           | industrial sponsor, who eventually ended up offering me a job
           | to build spacecraft before I finished the PhD itself (which
           | was a little complicated in itself), which I took.
           | 
           | After I started with them, I basically apprenticed under an
           | experienced AIT engineer who was coming up to retirement.
           | This is where I really learned a lot. If you ever get the
           | chance to work under someone in the later stages of their
           | career, you really can learn a lot from them.
           | 
           | That was at OHB Sweden, which was an excellent place to see a
           | broad range of things in the industry. I go to work on
           | multiple spacecraft and various stages of development, from
           | proposal, to qualification, to final assembly and test, and
           | to launch as an operations engineer. Really a super
           | experience I am not sure I could have been luckier ending up
           | there.
           | 
           | After that I joined a very small team building the ispace
           | lunar lander, which I am fairly certain will remain the
           | pinnacle of my career. Never have I worked with such a great
           | team on a great project. Everything just worked between us,
           | and a small team really achieved something spectacular (even
           | if it ended up in a crater on the moon).
           | 
           | Now I am working in Ireland for a data acquisition system
           | developed for flight and launch vehicles. Learning the ins-
           | and-outs of ethernet communication and analog circuitry. So
           | far my complete lack of understanding of electronics hasn't
           | been a problem, somehow.
        
         | mechhacker wrote:
         | In my brief stint working on spacecraft in the private sector I
         | worked with guys like you that did beautiful things with wiring
         | that I loved to see.
         | 
         | I hear you on scheduling too. I've given best estimates and
         | they then get chopped up and halved (or worse) by management
         | types, then things start to slip and we end up being closer to
         | what was originally estimated, but somehow everyone then gets
         | surprised.
        
           | cuSetanta wrote:
           | As you say, things shift around, promises get made,
           | everything gets delayed and all of a sudden there is no
           | margin left. Unfortunately AIT has to do all of the hardware
           | work with no margin so much of the time.
           | 
           | Secretly I love the power that can give us. You can shout at
           | me all you like in the meetings Mr. ESA engineer, but if the
           | holes don't line up, I cant put a bolt through them. Nothing
           | quite like drilling holes in spacecraft on the launch pad.
        
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       (page generated 2024-06-02 23:00 UTC)