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Build a CubeSat
Швейцария
Добавлен 25 дек 2023
CubeSat EPS v1: Assembly
#PCB #assembly is a tricky beast, but this one went reasonably well - right until the last second… It’s been a thrill, to say the least.
Huge thanks to @PCBWay for sponsoring this video!
Use my referral link to get $5 credit and support my quest to build a #cubesat :) pcbway.com/g/i2s1I5
*PSA*
I am taking a break from uploading new content until February 1st, 2025! Thanks for sticking with the channel through the first year and hopefully see you next year!
*Timestamps*
00:00 Intro
01:02 Overview of PCBs
03:33 Solar Charger Module Assembly
04:29 Buck Regulator Module Assembly
05:20 EPS Pasting
06:40 Materials used (paste, flux, tools)
07:06 EPS Placing
04:40 EPS Reflow
08:57 Results
09:28 EPS Assembly De...
Huge thanks to @PCBWay for sponsoring this video!
Use my referral link to get $5 credit and support my quest to build a #cubesat :) pcbway.com/g/i2s1I5
*PSA*
I am taking a break from uploading new content until February 1st, 2025! Thanks for sticking with the channel through the first year and hopefully see you next year!
*Timestamps*
00:00 Intro
01:02 Overview of PCBs
03:33 Solar Charger Module Assembly
04:29 Buck Regulator Module Assembly
05:20 EPS Pasting
06:40 Materials used (paste, flux, tools)
07:06 EPS Placing
04:40 EPS Reflow
08:57 Results
09:28 EPS Assembly De...
Просмотров: 3 609
Видео
CubeSat EPS v1: PCB Design Review and Challenges
Просмотров 4,6 тыс.2 месяца назад
After some trials and tribulations, it's my pleasure to share with you the first (and flawed, but hopefully functional) revision of my #cubesat EPS #pcb =) Thanks again to @dario_fresu for providing feedback! Definitely check out his channel if you want to learn more about PCB design. *Timestamps* 00:00 Intro 00:30 Board Overview 01:53 Battery Connection Pins and Jumpers 02:59 Back Side 03:25 L...
Structure Update: Panels, Connectors, Magnetorquer Ideas
Просмотров 5363 месяца назад
In today's video we talk about how my #cubesat's #structure is coming along in #cad Solar and other panels, brackets, the EPS PCB, experimental connector stuff, and potential future magnetorquer ideas. *Timestamps* 00:00 Intro 00:31 EPS PCB Envelope 01:02 Solar Panels and Connectors 01:55 Experimental Receptacle Usage 02:44 Center of Mass Adjustability 03:32 Other EPS PCB stuff 04:40 Experiment...
CubeSat EPS v1: KiCad 8 Schematic, Part 2/2
Просмотров 7404 месяца назад
In this video, we finish our #kicad #schematic walk-through of my #cubesat Electrical Power System v1. If you haven’t seen the first part, here it is: ruclips.net/video/YYE7vHrqCd8/видео.html This time around we mainly talk about connecting the #eps to the side panels (where the solar cells are) and to the rest of the system. Also, I will tell you about how I plan to make the battery chargers a...
CubeSat EPS v1: KiCad 8 Schematic, Part 1/2
Просмотров 1 тыс.4 месяца назад
This is the first version of the Electrical Power System (#EPS) #schematic for my DIY #cubesat done in #kicad 8. In this video I walk you through most of the components I chose and how I try to achieve some resilience through redundancy and a bunch of telemetry. If you have any suggestions, please let me know. I’m new at electronics design, so I am more than happy to learn from you all :) *Time...
CubeSat EPS: Breadboard Prototype
Просмотров 9845 месяцев назад
In this episode we find out if the main components I picked for my #cubesat EPS actually work together by hooking up some eval boards to a @raspberrypi Pico W on a breadboard. *Timestamps* 00:00 Intro 00:25 Solar Cells 01:35 Battery Charger 02:15 Buck Regulator 02:46 3V3 Regulator and RBF Jumper 03:36 Dashboard and PMBus Struggles 06:16 Charging Test 07:06 Discharging Test 08:36 Next Steps and ...
CubeSat EPS: Block Diagram and Part Selection
Просмотров 1,7 тыс.6 месяцев назад
My first step towards designing an Electrical Power System for my #CubeSat (or #EPS for short, aka. BMS or Battery Management System) is to make a simple #blockdiagram and then select some parts that are easy to work with. The great @RGSAT is my inspiration for this, but I take a slightly different approach. All of this is in preparation for breadboarding and schematic capture, which I will cov...
Connecting the PCB Stack in my CubeSat with M.2
Просмотров 8416 месяцев назад
In this side note we explore how M.2 connectors could be used to connect the PCB stack in a #CubeSat. This idea is heavily inspired by #MicroMod by #SparkFun - that's why I call it MacroMod for now, but please do suggest a better name, I beg you. *Timestamps* 00:00 Intro 00:09 #PC/104 01:19 SparkFun MicroMod 02:35 MacroMod 04:30 Daughter Boards *Links* @sparkfun #MicroMod www.sparkfun.com/micro...
CubeSat Structure: EPS Bay
Просмотров 5827 месяцев назад
In this episode we are taking a look at the #EPS compartment of my #CubeSat, basically where the batteries and the battery management system will go. _Timestamps_ 00:00 Intro 00:35 EPS Bay Tour 06:00 Cost 07:00 Battery Contact PCBs Thanks to @Snaptron for the contact dome samples and @PCBWay for once again doing a good job! (not sponsored) _Repo Links_ EPS Bay CAD files in the Structure Repo: c...
Battery Selection for a CubeSat EPS
Просмотров 9748 месяцев назад
What do you need to take into account when choosing batteries for the harsh conditions of launching to and operating in space? Find out as I share my journey into the rabbit hole of #18650 #lithiumbatteries and learn how the @NASAJPL saves the day once again. *Timestamps* 00:00 Intro and Requirements 00:57 What's UL-listed? 01:31 Choosing a form factor 03:57 Choosing a chemistry 06:48 Where to ...
Direct to Cell Technology in 2024: A Quick Summary
Просмотров 3,3 тыс.8 месяцев назад
Direct to Cell Technology in 2024: A Quick Summary
CubeSat Structure: From Idea to Mockup
Просмотров 5299 месяцев назад
CubeSat Structure: From Idea to Mockup
Launching a CubeSat to Space: Rideshare Missions Explained
Просмотров 43210 месяцев назад
Launching a CubeSat to Space: Rideshare Missions Explained
CubeSat Standard Read-Through: Electrical Specifications (Part 2 of 2)
Просмотров 49410 месяцев назад
CubeSat Standard Read-Through: Electrical Specifications (Part 2 of 2)
CubeSat Standard Read-Through: Mechanical Specifications (Part 1 of 2)
Просмотров 81711 месяцев назад
CubeSat Standard Read-Through: Mechanical Specifications (Part 1 of 2)
Specs and Scope of my CubeSat Mission
Просмотров 1,8 тыс.11 месяцев назад
Specs and Scope of my CubeSat Mission
Developing a DIY CubeSat: Where to Start
Просмотров 3,8 тыс.11 месяцев назад
Developing a DIY CubeSat: Where to Start
Deez nuts
Great to know that I function in the same was as a cubesat deployment switch - 1:39
😂😌 same
As far as I heard some rumors when it was announced, the DTC from starlink aims to do some "magic" and appear as virtual stationary BTS for cell phones that are at least LTE capable, so that the speed of satellite could be eliminated and no extra hardware needed for the phones.
Super interesting! It remains to be seen if and how this would work for a satellite at a similar altitude but with different inclination.
oshpark is typically better for boards @PCBWay
Are you able to make a gerber file of a board to mine crypto currency?
No
Hey what software is this? and is it same for your satellite design or these are two different software for designing satellite design and pcb design?
That's KiCad. It's an open source software for electronics design. You should check it out, there is a ton of tutorials for it on YT.
🔥🔥🔥🔥
Hey your what you are doing is really inspiring for me. I am also doing something like this. Please keep doing what you are doing and share as much as possible. You got a new subscriber.
Thank you! Will do!
I'm a little late to the party (I just discovered your channel today), but I'm looking forward to watching the rest of this project. Your enthusiasm for learning how to do something this big is just awesome! I wouldn't normally comment on a video that's three months old but since you're still a decade from launch, I'll add a few thoughts... 1. From an electronics design standpoint, you may be putting the cart before the horse by designing the EPS first. A smarter approach might be to set aside a volume for the EPS, then move on to the compute, comms and payload. Once you've got a fairly good idea what kind of power demands you have, you can come back to the EPS and make smart decisions to satisfy those demands with a sensible amount of headroom. That way you might avoid selecting parts like the LTM4675, which is likely wildly over-spec (and over-priced!) for your needs. 2. Your desire for redundancy is understandable, but be careful not to take it too far. For example, putting four pull-up resistors in parallel is... a bit much. Keep in mind that four 100kΩ resistors in parallel equals a 25kΩ pull-up. When that line is held low, you're burning four times more current than a single 100kΩ resistor. If that scheme is replicated multiple places in your design, the current draw can add up. If you want redundant pull-ups, consider testing to figure out the highest value pull-up that will reliably work with an IC, then use a couple resistors of that value. I would be very surprised if you find any IC that won't work reliably with 1MΩ. 3. Resistors are probably the single most reliable component you're going to use. The most likely cause of a pull-up resistor failure will be PCB flexing. If multiple redundant resistors are mounted next to each other, then any PCB flex will affect them all. They're more likely to effectively function redundantly if they're dispersed, but that complicates PCB layout. 4. Speaking of pull-ups and pull-downs, don't forget to include them when calculating your power budget. They're often overlooked and can wreck the performance of battery-critical designs that fail to take them into account. 5. Are you sure that using the RBF and Deploy switches as LDO enable pull-downs is OK? When the CubeSat standard says "fully inert and batteries disconnected," it likely means that the battery is completely isolated from the electronics (i.e. BAT+ goes through the switches, then to the EPS circuitry, so there's no power on the board until the RBF pin is pulled and the Deploy switch is closed when the vehicle is ejected from the dispenser). The way you appear to have it designed now, the battery is always connected to the EPS board and all of those pull-up resistors -- held low by the grounded RBF and Deploy switches -- will burn power from the moment the battery in installed. 6. I was going to make a comment about the difficulty of working with LGA/BGA parts, but if you've used BGA in the past, then you already know what you're getting into. I'll just point out that the more common, "jelly-bean" parts that you use, the easier and cheaper it will be to iterate prototypes. How many revisions of the EPS are you willing to build with nearly $75 in just two μModules (not to mention all the passives, load switches, ADC, I/O expander, etc.)? For someone who's new to all of this, you're doing amazing work so far. Best of luck!
Hi! Thank you so much for taking the time to write all of this - that's awesome! Detailed feedback like yours really is invaluable to me. Basically, I agree with all of your points. Here are some of my thoughts for context: 1. Yes, if I were to design for one specific application, it would make more sense to do it the other way around. My thoughts here were: A) Other people may want to do different things with these designs, so let's over-spec this on purpose but make it modular so more sensible folks (like yourself) may want to design more sensible charger and buck modules. I don't know if you are aware of this, but the μModules are themselves on stamp-sized modules for that reason. B) RGSat started with the EPS, so it must be right way to do it ;) 2., 3., and 4. I lol'd at the "..." xD True, and in hindsight, I was clearly overdoing it due to a lack of experience. I just wanted to avoid a single point of failure due to a $0.05 part, but I will change it in r2. Regarding power dissipation, I calculated something like 9 months of "waiting for launch and deployment time" (I am sure there is a proper word for this) for the power used by the bias resistors, but that doesn't factor in battery self-discharge. So optimizing the resistor values will be the first step when I get to optimizing power use in general. 5. I'm in fact not sure, but what would be the alternative to using a MOSFET? I'd like to avoid a mechanical relay for volume and vibration reasons. How would you design this? 6. Yeah, that's another thing I am unsure about. On the one hand, I suspect that non-BGA components will go the way THT went sooner or later, so it kind of makes sense to get used to working with BGA. On the other hand, accessibility and cost are major considerations. I am willing to spend a good part of my income on this project, but in the end, I want it to be as accessible as possible. There is a balance to strike there, I think. Again I really appreciate you taking the time to share your thoughts and I hope to continue this exchange in the future!
Amazing, will be following your journey till the end.
Thank you and welcome aboard!
In terms of Inhibits: Don't use mechanical relays if possible - most Spacecraft standards strongly recommend against COTS relays, as they are not vibration and shock tolerant. Any hardware inhibit (so also MOSFETs) should count
Thanks for commenting! Yeah, mechanical relays seem like a bad idea in a high vibration environment. I am currently using 4 MOSFET load switches for redundancy in the first version of the EPS design.
Keep the videos coming. I've had the idea of working on a CubeSat for a couple years now and I recently (more like "finally") starting the actual work on realizing a part of it; a BUS. Well actually my first prototype design is going to be much more general, as in its my first time making a pcb that complex, but it's time. So in other words, I'm designing a development board for a BUS at the moment. Hopefully, since Mark Rober published a video about a CubeSat, you might get a boost in views/subscribers!
Nice, that's great to hear! If you feel like sharing, I'd like to follow along with your project. I think RUclips needs more CubeSat content :) I wasn't aware of that Mark Rober video, will be interesting to see if it has some spillover effect.
Be careful some manufacturers prohibit use in a satalite
Hi there! This design is going on a high altitude balloon at the most, but that's good to know for future, space-bound versions. Were you referring to any specific component?
@@buildacubesat nearly all due to import and export regulations and other things hence why they cost millions also sometimes the altitide limit is there to prevent missile use
@@UKsystems Ok, I see what you mean. So when I order components from Digikey and Mouser, I have to state the intended use before I can place the order. There, I always clearly explain that I will use the parts for prototyping a CubeSat and so far, my order always went through. So this should be fine. It is true that some dual use technologies like GNSS receivers and bolometers are limited for civilian use (altitude and speed limits for the former, frame rate for the latter). When purchasing the unlimited variants, you have to fill out some more paperwork and supply more context about your use case. Usually there is some back and forth with the vendor, but so far I have not run into trouble with that either. But thanks for having my back.
@ the issue is when it randomly applies to a resistor
This is so GOOOD!!!🔥
Haha I'm super happy that you like it 😄 Thanks again for coming on board!
@@buildacubesat We love it so much! Honored to be a part of your campaign! 🥳
There's an open source firmware for the MHP30 called IronOS that supports reflow profiles with up to 5 phases / steps.
Awesome! Thanks for sharing, I will install that
just the other day I was thinking of designing one just to build and test with than I found your videos and I thinks its just better to live watching your content than try and build one my self. Very excited to watch!
Thank you, I am happy to hear that you enjoy watching this series! What you said there is exactly what I thought a couple of years ago when I discovered RGSat's channel =) So if you ever decide to start your own project after all, feel free to share! 🛰
Awesome to see that PCB Way sponsored this video!!!!
One thing I noticed is pcbway isn't going just for sub count they are actually funding really good projects
@@awdhut-e2ethey own the files so they have something to gain
@@UKsystems anyways most of the creators open source the files , but it's really great for small creators with limited resources , they want to do something big so viewership increase and they get more money but because there is no viewership so there is no money and no big project So someone is breaking the cycle
@ it is a requirement for sponsorship by them
@@UKsystems Slight correction there: All design files are open source and freely available on the Codeberg repo (there is a link in the description). So transfer of ownership is not part of the sponsoring agreement I have with PCBWay. Of course I can only speak for my channel, so maybe you have had different experiences.
... беженец ???
I don't know what you mean by that...?
@@buildacubesat ...are you Swiss by birth?
@@ostrov11 I am
@@buildacubesat ... I'm sorry, I thought you had a Ukrainian accent.
No worries :) That's just a pretty thick Swiss-German accent
I feel your pain at 8:03 😥. But overall very well explained video 🤘.
Great video! Looking forward to february! :)
I'd love to see what feedback www.youtube.com/@PhilsLab had of your layouts. He's a true master of small, digital design.
Yes! I am planning to reach out to him about a collab in the future, when the design is a bit more mature (r2 or r3).
OK, the directives that Dario gave you are very good, stitching via is easy, one GND go really next to each high speed signal via, that is all. The size of the via is the same as what you are using for the signal. And you do have to remove whatever is on layers 2 and 3, unless you know when, you should not put anything there. On a 4 layer board you can use 18mil of distance between high speed lines . All digital lines should be considered high speed unless you are clear otherwise. Analog lines are low speed, except RF. Don't forgot to put a decoupling capacitor, you can used 10uf 0402 and you will be ok. And forget about layers 2 board, use only 4 layers.
Thank you for taking the time to comment! Yes, there is a lot to improve for r2. Two questions: Is there a reason why you would prefer 0402 over 0603 as decoupling caps (other than limited space)? And you would even go with a 4 layer board if the layout is feasible on 2 layers? For EMI performance or are there any other reasons? Thanks again!
MPS has a really nice line of highly integrated, inexpensive switching power supply-in-a-chip ICs. They include the inductor and all you need to do is add some capacitors. MPM3620 is the part number.
This looks like a really good fit - and that thing is tiny! Thanks for sending this my way, much appreciated.
One tip: you will need a batttery balancer IC for the cells in series. Parallel cells of around the same capacity will share charge so they don't need balancing and can basically be treated as one cell, but series cells will need a balancing charger.
Yes, that's definitely on the roadmap for v2! I want to get the basics right first, so for the moment (up until the suborbital balloon flight next year), I am just using equally charged cells. Are there any balancer ICs you can recommend? As usual, there is a staggering variety.
@buildacubesat I don't have any recommendations, but projects like OreSat, PyCubed, and PROVES probably use some useful ICs (and they've already been tested in space).
About the BGA routing, check if there are layouting application notes. on 0.8mm pitch BGAs dog-bone fanout should work, lower than 0.6 via-in-pad is probably neccessary. Since ease of service and ease of soldering is a priority in my Formula Student project we just avoid BGAs alltogether, so i dont have any practical experience with BGAs
Thanks! I should probably have thought of that myself after spending hours looking at these data sheets for the schematic xD Turns out there actually are layout examples for both uModules I used. So in r2 I will probably go with those... I just assembled the first charger PCB this afternoon, going to test it tomorrow :)
from my formula student experience with CAN bus, i think the non-differential pair routing is not much of an issue, CAN bus is fairly robust and as long as you dont have a lot of EMI (like in a self made EV for example ^^) i would assume its fine as-is.
Ok, that's good to hear! I'm really looking forward to putting this to the test though.
Looks amazing man! love seeing the progress
What a beauty 🔥
I know, thanks. I have been working out lately.
congratulation for 1K subscribers
Thank you very much! I didn't think this would happen in the first year of this channel
Thanks for the shout-out, Manuel! Glad you found the tips useful. :) Good luck with your project! Best, Dario
@Build a CubeSat PGB1010603MR has a Clamping Voltage = 150 V. This could be a problem if for example voltage is 70V. No problem if voltage is more than 150V. Why did you select this device?
Hi! Thanks for bringing this to my attention, that's really helpful. I have some of them at hand and didn't check the specs closely enough. I don't expect anything above 24V anywhere on the board down the road. Is there a 0603 device you would recommend?
schöns projekt
Merci :)
nutzisch du github?
Nö, i ha aues uf Codeberg, isch a zimlech sympathische Verein us Berlin. D Links si aube ir Beschribig.
Sub #908 Baby!!
Haha thanks man =D
Thanks for sharing. What version of kicad are you using coz I see it supports dark theme
Thanks for watching! I am using 8.0.6 and the theme options are located in Preferences -> Preferences... -> PCB Editor -> Colors
This is the sort of channel we need more of on YT. Sharing information about more advanced projects and applications. Looking forward to the future videos.
Building REV 2 for my EPS set to launch next year. Thanks for the valuable insight into your design
Awesome! Just watched your NASA ASCEND video, beautiful footage. Are you going to document your next launch too?
plz we need a detailed series on how to make an EPS for cubesat.
I'm on it :) there are two videos about the schematics and one about the PCB layout on my channel right now
@@buildacubesat Thankyou, it will be a great help for Electrical engineering students.
I think some people may use the Cubesat format for ballon flight - to start being familiar with the architecture. That may explain the presence of sensors related to the atmosphere
Good point! I have done that myself multiple times. It may be beneficial to advertise the purpose of such sensors more clearly though imo.
9:02 i think you're misinterpreting "unspecified signal impedance requirements", you say it's not applicable to your signals that don't have controlled impedance requirements, when that's exactly what that condition is referring to. this is saying "for signals that don't state a specific controlled impedance requirement, aim for 50 ohms", or in other words, most of the signals on the board. I'm far from an EMI expert (just a hobbyist), and I def find controlled impedance intimidating too, but there are online calculators you can use, they ask you for a bunch of info about the stackup (which should be available from your fab, in fact a lot of fabs have their own calculator that inputs this data for you), whether the signal is single-ended or differential, and your desired impedance, and it'll tell you the trace width and spacing (technically, you pick a value for either width or spacing and it gives you the other one, then you fiddle with the values till you get something that fits well into your design). No idea if the advice to use 50 ohms by default is valid, but given how harsh the environment is up there, it seems reasonable to me to have *some* default controlled impedance for non-specified signals. also: controlled impedance is weird, because you usually have some amount of unavoidable discontinuities in the trace impedance. unless the chip package, connector, and any other components in the signal path have been designed specifically to perfectly match your board stackup, the geometry of the pads probably won't perfectly match the width/spacing needed for your stackup. if you wanna get really fancy, you can smooth the transitions between the non-ideal pad sizes and the correct trace sizes, but there's gonna be a couple mm here and there where the impedance is a bit off. (not to mention the connectors themselves, take a look at ethernet for example, the spec's maximum cable length is predicated on a maximum number of jacks it can pass through because each jack is a discontinuity). As far as I can tell, this seems to just be accepted and budgeted for in signal integrity requirements, but i don't know the specifics of how that works / how to calculate whether you're within tolerance (especially since in space your tolerances are probably more strict than the official spec!) I would expect all the signals on the board (definitely i2c, probably CAN as well) to work just fine, and the issues will be in emission of and susceptibility to EMI, and possibly error rate if you're driving the CAN bus rly fast. so, stuff you def need to fix before flight but will likely work well enough for initial tests. i2c especially should be functional, as long as the actual circuit is correct and you're not driving the clock in the MHz. and if i understand your CAN pass-through correctly, you have maybe a few mm of track total that the signal passes through, so the size of the discontinuity is pretty small (in a lot of designs i've seen, there's usually a couple mm of wrong impedance breaking signals out of a footprint). no idea how that discontinuity scales across multiple boards stacked together though, that might add up to a problem.
Hey! Thank you so much for taking the time to comment in this level of detail, this is super helpful! I did understand the "unspecified signal impedance requirements" in the same way you mentioned - it's just that I don't always succeed in expressing myself coherently in these unscripted parts... I appreciate you mentioning this though. So for r2 I will definitely look into impedance control and use the approach you suggested (get in tha ballpark using online calculator and then tweak track sizes and spacings to fit in the design). That's an interesting vantage point, I have never thought of connectors being much of a problem for SI, rather cable/trace length between them and EMI. So I suppose in my design, the limiting factor may actually be the number of M.2 connectors a signal may go through in the stack up. Interesting! I dont' plan to run anything in the MHz range. For I2C, the usual 400 kHz mode will be plenty I think. You also brought up something I read a few times now, but never quite understood: Why do you think LEO would be a harsh environment regarding EMI? Would ionizing radiation (solar / cosmic background radiation) have an influence? Because thinking about just how empty it is up there, it would seem to be a much more benign environemnt regarding EMI than say an average office building. About smoothing transition between pad sizes and traces: Would you tend to step-up trace widths (like Phil Salmony tends to do) or use teardrops? Thanks again for the input. I will start a Discord next season, would be awesome to see you there :)
@@buildacubesat so to be clear this is all just anecdotal advice from my relatively limited experience as a hobbyist. my main assumption around stricter requirements in space is just, a vague sense of "radiation" being a problem, and the much higher cost of failure, since a lot of otherwise recoverable or easily fixable error states are potentially mission-ending when you can't physically access the device. i think what you're saying about it being much quieter up there is probably true, and ionizing radiation is a totally different thing from EMI, so i'm likely overstating the problem, i guess i was mainly just going off the general association between aerospace and stricter standards. I have not done any research into transitioning btwn trace sizes, my main intent was just to point out that lots of applications seem to get by with just accepting those small discontinuities. but i definitely think it's worth exploring how to optimize that, i just don't know much about that myself.
my intuition would say test your i2c bus at 400kHz, but also some much lower frequency (whatever the lowest your application can afford is) and use that in the final version, just to give you a nice big margin of safety. also: some of i2c devices implement CRC checksum functionality, you can check for that and make use of it where available to give you extra assurance
@@spambot7110 Sure, I understand that and your comments are still very much appreciated :) I want to look more into EMI/SI for space next year and ideally have a CubeSat dev as a guest on the channel who may be able to share some insights. For now, until the high altitude balloon test flight in June, I am going with a 'good enough if it works' approach to keep the momentum going, and then after that, I will start going over each subsystem with a fine-toothed comb and move into a space-worthy design direction. Well-reasoned comments like yours will be great to refer back to in the future, so thanks again for taking the time.
@@buildacubesat oh i just thought of something, when you see the length matching squiggles in a trace, when it's a differential pair of traces and the squiggle is on just one of them (for skew correction), that's another impedance deviation. so, i still don't know how to quantify it, but clearly there's a way to budget for it
Nice videos. U motivated me to try and learn more about CubeStas! Laptop specs?
Hey and thanks for the comment! I'm happy to hear that :) This is a framework 13", with the 12th gen i5. I can really recommend framework laptops, definitely check them out
out of everything, your CAN will most certainly work. I have people using seen untwisted wires for can bus and they work just fine for small node lengths. if you manufacture this with JLCPCB they wont charge you for via in pad service. I dont know about others, but as this is going on a satellite you might have to go to other vendors that uses more exotic materials and process to manufacture pcbs. but for one off prototype JLCpcb should be sufficient. Listen to the recent podcast from The Amp Hour, its on cubesat.
That would of course be great, I'm eager to find out! =) I sent this to PCBWay for manufacturing (they also make all the CNC parts) and you're right, for flight hardware a different substrate may be needed (they also offer Rogers). But that's still a few years away :) Thanks for the comment and also the telling me about that TAH episode, will definitely check it ou!
Hey man, I've just found your channel, and as an electrical engineering student that wants to get into the space industry a lot more, I want to thank you for these really good and information heavy videos! I've been binge watching your videos and have come to learn a lot of interesting information on things that I had no idea about, and have seen a lot of crucial problems when making cube sats. Thanks again for the videos and please keep making them :)
Hey! Thanks so much for the kind words, that means a lot =) It's great to know that this stuff is useful for someone getting into the space industry. Best of luck with your studies, and I'll definitely keep the videos coming! Feel free to drop any questions or topics you'd like to see covered in future videos
You made micromodule out of micromodule, :D. Will the buck module with parts on both sides fit into the hole on main board? Looks very nice overall.
Yeah basically, babushka-style xD Thanks! Yes, I placed all components in a 20 x 20 mm area, so if I didn't mess up too badly, this should work.
aw hell yeah, another cubesat channel. Rg sat kind of went MIA so there is potential in this channel. Im planning on starting an organzation where we build a cubesat at my university and I like watching stuff like this, so keep it up!
Hi! Great to hear that you are starting a CubeSat project - no better time than the present if you ask me :) Are you going to open-source it too? I got in touch with Richard from RGSat a while back and he mentioned being super busy with work, but not having abandoned the project. So I'm keeping my fingers crossed for him to continue at some point.
@@buildacubesat Well I'm glad he didn't quit. But yeah, I do plan on making everything open source, even the ground station. I think open sourcing things like this especially the flight computer is good for the community considering commercial products are so expensive.
@@mdarnell321 100% percent agree! Make sure to send a link to your project my way, would love to follow
Man! I really appreciate your content. Keep it up!