Chuck,
Forgive this long email...
SInce everything is interrelated the only way to deal with it is
from a system engineering perspective (in my opinion). You can't
design the various subsystems with each group working in a vacuum. If
you do, this is what happens.
For example: I've researched the maximum amount of bending that
should be allowed on a SMT circuit board. AVX, the capacitor
manufacturer, suggests a maximum bend radius spec for SMT circuit
boards of 60 inches. That works out to 0.0084" maximum deflection over
any 1" segment. That's about the thickness of three sheets of paper.
The tolerances of the existing sheet metal enclosure with separate heat
sinks and multiple swaged-on stand-offs is way too loose, by at least
an order of magnitude. The enclosure I have is also warped and
flexes. To me that means we need a milled enclosure...
If we're going to do that we might as well do it right and make
it into two separate cells with noisy digital circuits in the front and
analog in the back...
If we do that then you probably don't have to worry too much
about radiated emissions or changing the PCB form factor or connector...
Filtering conducted EMI would rise to the top of the list of
concerns. Moving the switching frequecies of all the supplies up as
high as possible would ease the filtering burden on everything on the
satellite and tend to push any spurs out of the passband. And so forth
and so on...
Once we had some hard data on the amount and characteristics of
the conducted EMI from the power distribution point, then John could
start designing in the necessary EMI filtering and CPB layout to fit
into the box and meet the yet to be determined EMI susceptability
requirement for the receiver. If his design didn't look like it would
be able to meet the requiement then there would be some push-back to
the power distrubution subsystem to clean up their radiated EMI, etc.
I guess the bottom line would be that since you can't know the
radiated and conducted EMI susceptability of everything that may end up
connected to the CAN-Do module, all you can do is try to make it as
clean as you can and get the switching frequency as high as possible.
By the way, I just looked up the Maxim converter you're using and it
looks like it's very lightly loaded which would explain wny its running
at 5 kHz instead of the 200 kHz they spec. I spent some time looking
for a better choice and couldn't find anything, but I don't know what
you requirements are.
73,
Juan
On 7/17/07, Chuck Green <greencl@mindspring.com>
wrote:
Hi
Juan,
I agree that specifications prior to design would be helpful
(required?). But as far as the EMI issues are concerned, we do seem to
have a chicken/egg problem. And I'm not sure it is practical to design
a widget that meets the requirements of receiver modules. Most modules
simply don't need anything nearly this good. But we should do
everything practical to accommodate receiver modules, and maybe meet
their requirements completely.
Thanks,
Chuck
Juan Rivera wrote:
> Chuck,
>
> My comments might have been buried in the flurry of email a while
back.
> Things seem a bit quieter now so here they are:
>
> 1) Don't get too far into a redesign until a top-level EMI
requirement is
> created. This can't be done properly until prototype solar panel
power
> converters are fabricated and tested. I would work to create a
new power
> supply with a switching frequency of at least 500 kHz while you
wait
> however. This will make filtering much easier, the filter
components will
> be smaller, and any spurs that make it into the receiver will be
outside the
> passband of the IF.
>
> 2) The EMI requirements for radiated and conducted emissions and
> susceptibility should flow out of that test data and not be
guesses.
>
> 3) Once we have an EMI requirement then tradeoffs need to be
considered
> between the CAN-Do module and the enclosure - one or two
compartment? Sheet
> metal or milled construction? The results of that tradeoff study
will
> determine how much room you have to work with, how much front
panel space,
> and how much shielding and filtering are required.
>
> If I had my way the enclosure would be a two-cell milled enclosure
with all
> the RF and IF exiting out the side of the rear cell. The CAN-Do
module and
> the Receiver switching power supply would both be located in the
first cell
> with feed-thru filtering in the common bulkhead between cells (all
digital
> power in the front and all analog in the rear). That would mean
that the
> CAN-Do connector would be the only connector on the front of the
case. If
> that were true then the only reason to change connectors would be
to save
> weight or increase reliability. It would also mean that the
existing CAN-Do
> PCB footprint would be fine as it is.
>
> In my presentation I will suggest that the next revision of the 70
cm
> receiver should be postponed until all of these issues are
resolved.
>
> 73,
>
> Juan
>
>
>
> -----Original Message-----
> From:
eagle-bounces@amsat.org [mailto:eagle-bounces@amsat.org] On
Behalf Of
> Chuck Green
> Sent: Monday, July 16, 2007 7:47 PM
> To: Louis McFadin
> Cc: Dave Black ((Work)); Dave Black ((Home)); David Smith; AMSAT
Eagle;
> Samsonoff@Mac. Com; Juan.Rivera ((Work))
> Subject: [eagle] Re: CAN-Do-Too! ??????????
>
> Thanks, Lou.
>
> I don't know of any reason not to use them either. Obviously, it
needs
> to meet our mounting configuration requirement so the new
mechanical
> design can meet the objectives I stated earlier. This means it
must
> mount on the edge of a PCB. I think the HD15-D has three rows of
pins
> so I'm not sure how this can work, but I haven't looked at the
various
> parts available so maybe this problem has been solved.
>
> If we are going to seriously consider using HD connectors I think
we
> need the blessing of AMSAT's VP of Engineering and the EAGLE
project
> coordinator. This would be true for any change that would be
pervasive
> in the satellite.
>
> I am a little disappointed that there have not been any comments
> regarding the changes I saw as being made with a new design.
> Additions/changes/questions/etc. I don't think we should do a new
> design without this discussion. Maybe people feel these issues
have
> been well covered in the past. If so, a simple "looks good to me"
would
> be helpful.
>
> And no one has stepped up to say they are well qualified and will
design
> a new power supply. Without this, I don't see a new design
happening,
> but maybe.
>
> And finally, I see that no one has dared touch the subject of parts
> procurement I raised.
>
> Obviously, most of these comments are really meant for the Cc list.
>
> Thanks,
> Chuck
>
> Louis McFadin wrote:
>
>> Chuck,
>> Mouser has a very large selection of D-sub connectors
including the
>> high density versions. Most are in stock.
>> I see no inherent reason for not using them.
>>
>> Lou McFadin
>> W5DID
>> w5did@mac.com <mailto:w5did@mac.com
>
>>
>>
>> On Jul 16, 2007, at 7:19 PM, Chuck Green wrote:
>>
>>
>>> I have had one experience with the high density D
connectors. They
>>> were much larger pin count than 9 or 15! After someone
absolutely
>>> insisted that we use them I did the board lay out. Turned
out that
>>> they were *totally* unavailable!!! I did the board layout
>>> again@#$%&^* using standard Sub-D's. That was a
number of years ago
>>> so I would hope things have changed. If someone is
absolutely
>>> confident they can obtain the parts we need then I'm not
at all
>>> opposed to using them (remember, I'm not volunteering to
do parts
>>> procurement for this project; this is a good time to use
someone
>>> that's good at parts procurement).
>>>
>>> While at Goddard for P3D vib test I noticed NASA
satellites using
>>> standard Sub-D's. That was also a few years ago. Anyone
know of
>>> High Density Sub-D's being used on other satellites?
>>>
>>> Chuck
>>>
>>> Bdale Garbee wrote:
>>>
>>>> On Tue, 2007-07-10 at 09:02 -0700, Chuck Green wrote:
>>>>
>>>>
>>>>
>>>>> The sub-miniature D connector series has served us
well. If anyone
>>>>> has *experience* with something they think might
be a better
>>>>> choice, we'd love to hear about it.
>>>>>
>>>>>
>>>> At the AMSAT annual meeting that was held near
Washington, D.C., a
>>>> couple of years ago (three?), someone approached me
after the CAN-Do!
>>>> talk that Stephen and I gave to ask why we weren't
using the
>>>> higher-density connectors that put 15 pins in the same
shell size as the
>>>> 9-pin version of the series we have been using... and
followed up by
>>>> sending me what looked like mil/aero-spec samples of
such a part that I
>>>> probably still have in my basement somewhere. I'm
sorry that I can't
>>>> recall at all who that person was, but it was someone
who claimed to be
>>>> using such connectors professionally with good results.
>>>>
>>>> At the time, we weren't likely to be redesigning the
units any time
>>>> soon, so I didn't take any action on this
suggestion. If we're going to
>>>> revisit the design and think we need more than 9 pins,
it might be worth
>>>> investigating higher density connectors like that?
>>>>
>>>> Bdale
>>>>
>>>>
>>>>
>>>>
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