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This file was generated by Descript 

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Hywel: Hello everybody, I'm your
host Howell Curtis, and I'd like to

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welcome you to The Space Industry by
Satsurge, where we share stories about

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the companies taking us into orbit.

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In this podcast, we delve into
the opinions and expertise of the

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people behind the commercial space
organizations of today who could

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become the household names of tomorrow.

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Before we get started with the
episode, remember you can find out

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more information about the suppliers,
products and innovations that are

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mentioned in this discussion on the global
marketplace for the space at satsurge.

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com.

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Hello there and welcome to
today's episode of the Space

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Industry Podcast by SatSearch.

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I'm joined today by some returning
guests on the podcast, Michael Seidel

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and Adrian Helvig from Global Electronics
Manufacturer and a SatSearch trusted

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supplier, Texas Instruments, a name
you're, you must be familiar with if

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you've listened to this podcast, but
also if you're anything to do with the

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space industry or a wide range of other
industries where Texas Instruments or

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TI as it's commonly known operates.

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It's great to have you both.

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Back on the show, really really interested
to hear more about the the work that

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tech, that TI is doing in space.

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There's always a lot of information
presented by the company about the

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different applications and components
and and how they can be used to

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improve missions that TI shares.

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So this is great.

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Now today we're going to be talking phased
array antennas and how they can improve

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both performance and flexibility, which
is, or versatility, which is increasingly

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important in modern space missions, as
we're seeing teams professionalizing and

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services, trying to try to get more value
and do more with the equipment and the

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resources and the people that they have.

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Yeah, I'm really excited to
get into this topic today.

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Now, we'll start by setting the
scene a little bit, many people in

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the space industry are increasingly
aware of how congested the RF

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spectrum has become and is becoming.

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And there's a few
different reasons for this.

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I wondered if Adrian potentially
could, explain why this problem has

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come about and what RF engineers
are doing or can do to mitigate it.

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Adrien: Yes, sure.

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Welcome everybody.

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Yeah.

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So I will be happy to answer that one.

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So the RF spectrum has become very
crowded for several reasons, really.

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And the fact is we need to, More
data and faster speeds, right?

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So the demand for available
spectrum simply has increased.

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In addition to that, there are also
many new application in services.

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Like for example, phone services, internet
services, or air observation satellites,

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like weather satellites, for example,
defense communication, those applications.

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I using up more of the spectrum.

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And let me also add one additional
point here about the low earth orbit

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satellites, because on the one hand,
you can think those are offering more

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data transmission opportunities for your
system, but at the same time they are

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also creating another problem, right?

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Because those satellites
are moving very quickly.

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Relative to ground.

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And this makes really hard to maintain
the stable communication link.

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Yeah.

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And now to deal with all those
issues, engineers, developers,

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they are developing new solutions.

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And to be very honest with you,
the one of most promising is the

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use of phased array antennas.

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So actually our topic today,
and this antennas can direct the

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communication beam electronically.

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without needing mechanical parts to move.

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And this allows really for
better use of available spectrum

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by sending multiple signals at
different angles and frequencies.

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And at the same time, this technology
helps also to reduce the interference

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and improves overall system efficiency.

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And In using the RF spectrum.

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So in summary, by using the phased
array antennas, the space industry can

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really benefit and handle the anyway,
very crowded RF spectrum much better.

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Okay.

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Hywel: Fantastic.

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Yeah.

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It makes sense as we've seen the
industry scale in that these, there's

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some very valuable areas of the spectrum
are under increasing demand, but yeah,

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when you explain issues like the.

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Leo satellites there, though,
the how hard it is to maintain

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those stable communication links.

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I think that really puts
this issue into perspective.

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And as you say, the phased array
antenna technology is seen as a

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really promising solution for this.

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As I mentioned in the intro to
the show let's Get into more

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detail on this technology.

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Now, as far as I understand, phaser
antennas bring two big benefits.

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The increased versatility because of,
as you mentioned, the digital beam

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forming or the electronic steering.

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And that I believe they can enable
greater bandwidth because they

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can operate with narrower beams.

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So I wonder if we could discuss this first
point and, please correct my inaccuracies

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if they are there, but yeah, I wondered
if Michael, if you could explain what

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digital beamforming is and what benefits
it can bring to space applications.

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Michael: Yes, I'm very happy to attend.

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This is definitely not trivial to
understand, but let me give it a try.

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Imagine you have several antennas,
not only one antenna, but you have

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several antennas next to each other,
and you really put them equally spaced.

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One.

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next to the other, right?

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And they form an array of antenna.

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That's either a linear array in only
one dimension, but they're next to

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each other, or you put them in a
rectangular format and have them in two

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dimensions spaced next to each other.

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But you have multiple antennas
and all these antennas, they

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send the very same signal, right?

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They just add up, they accumulate and
form altogether a, now a a radiation

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characteristic with a single beam
but a more focused beam than if

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you have only a single element.

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So that's the first thing we have to put
there to get a more narrow, more focused

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beam, because you're accumulating the
characteristics of multiple antennas.

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together.

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And the second one, and that's
actually a pretty interesting even

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fascinating fact happening there.

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What people do now is they put a
delay where you're saying all antenna

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elements send the same signal.

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They do send the same signal, but each
one a little bit later than the other one.

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So you put this constant delay on
each one of those next to each other.

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And then the interesting
thing, what happens then is

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then the angle of radiation.

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It changes its direction, like
the very front is moving in

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a different direction then.

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And really controllable by the delay
you apply to each of these elements.

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And that makes now this antenna
steered purely based on electronics.

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So no mechanics involved.

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And that is of course a big benefit
that if you don't have to send

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many mechanics to space, that
is of course a major advantage.

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And now the.

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The next level of interest is like
you have, you can have this steering

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of the beam you're radiating.

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You can differentiate between frequencies.

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So you have one carrier frequency
getting one set of delays and

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the other carrier frequency
getting a different set of delays.

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And with that, you have now two
beams of different frequency

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pointing at different locations.

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And this is where you can now put groups
on ground, user groups on ground together

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and give this one group one carrier
frequency in one direction and the

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other group another carrier frequency.

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And this is how you divide up the
spectrum very effectively and with

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a very focused theme where you
accomplished on the best signal to noise.

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ratio on these user groups.

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Hywel: Really interesting.

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So it's almost as if you're operating
with two different antennas physically

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pointing in two different directions,
but you aren't, you're using the same

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one that's electronically pointing
the beam in different directions.

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Interesting.

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And then What about the achieving
the increased data rate by

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operating with narrow beams?

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How does this aspect of things work?

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Adrien: Yeah, so that, that's
really another aspect of using

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those phased array antennas.

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Let me try to explain.

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Achieving those increased data rates
by operating with narrow beams, Works

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because this better focused antenna beams
ensure that the transmitted signal arrives

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at the receiver with greater strength.

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And when the signal is
stronger, it improves so called

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signal to noise ratio, right?

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And this means there is less interference
and the received signal is clearer.

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And this clearer signal allows
simply for higher data throughput.

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As more information can be transmitted
accurately and efficiently.

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So thinking about this, those narrow beams
are really essential in, in boosting data

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rates and and making the communication
link more reliable and robust.

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Hywel: I see.

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That makes sense.

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Okay.

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Okay.

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Yeah, got it.

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So we have these, we have this technology,
the phased array antenna technology.

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It provides these certain benefits around
increasing the data rate and so on.

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We mentioned that the RF spectrum
is, Gary, particularly crowded.

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Therefore, this kind of technology
is needed, but to bring it to home,

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to the so that space engineers and
mission designers really understand

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what value this technology brings.

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I wonder if you could
give some examples of.

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different space applications and
services that would benefit the most from

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using phased array antenna technology
and why that would be the case.

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Adrien: Yeah.

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Yeah.

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So there are really many and I
can try to list some of them.

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In general, phased array antennas would
really greatly benefit in would greatly

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benefit any space application that
relies on high data transmission, right?

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So the best example here is
telecommunication services.

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Why?

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Yeah, because they need high data rates.

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Another example could be
rather imaging applications.

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Those application would also benefit
from this because they need very strong

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focused beams for accurate imaging.

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And there is also another
aspect I wanted to talk here.

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Those more focused beams helps also
to reduce the transmit power, right?

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And this makes the whole
system much more efficient.

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And now in the beginning, we were
talking about the challenges of low

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earth orbit satellites and their
rapid movement relative to ground.

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So now with the phased array
antennas, They can quickly adjust

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to compensate for those rapid
movements and this ensure again the

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reliable communication link, right?

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So overall, those phased array antennas
improve your performance, your efficiency

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and reliability across really a wide
range of space application and services.

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Hywel: Okay.

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Makes sense.

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But of course.

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We always try and address this when we
talk about space engineering, missions

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in space are all about compromising.

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You mentioned, as you mentioned
earlier, the, we can't send

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mechanics into space to fix things.

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There are unique limitations
placed upon any technology.

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because of the extremes of
the operating environment.

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So my next question is, how is the
swap C budget of a mission affected

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by using phase array antennas?

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And what can engineers do to
deal with the, I would guess,

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inevitable trade offs that would
occur by using these technologies?

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Michael: Yeah.

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Yeah.

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I think first off, I think you suspected
already looking at the number of

00:12:34.240 --> 00:12:39.225
elements, the, Amount of electronics
and the cost and the power budget and

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the size and the weight all goes up.

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So your swap or the size, weight and power
and cost budget is that the first plan

00:12:47.305 --> 00:12:52.575
compromised, but what you get in return
is, of course, the amount of data rates

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and the amount of data rate per user.

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You accomplish with it, and
that really matters, right?

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And this is where the ratio
improves a lot, right?

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So it's absolutely worthwhile
going there in this direction

00:13:05.080 --> 00:13:06.860
by increasing the data rate.

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And we said it before, right?

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No need for mechanical steering
is, of course, also very important.

00:13:12.180 --> 00:13:15.330
Good benefit, important benefit,
and it's super fast, right?

00:13:15.390 --> 00:13:20.020
As we move over ground very fast that
is where these electronically steered

00:13:20.090 --> 00:13:24.360
antennas help us very much with
the big challenge that is probably

00:13:24.410 --> 00:13:25.980
will always be around with us.

00:13:25.980 --> 00:13:28.870
We put a lot of electronics
in a very dense area.

00:13:29.460 --> 00:13:32.660
And that is where the challenge is.

00:13:33.590 --> 00:13:37.900
And of course, the amount of electronics
and the complexity increases the cost.

00:13:37.900 --> 00:13:41.460
But this is where the good news
is that meanwhile, the electronics

00:13:41.480 --> 00:13:45.810
industry and semiconductor industry
has come up with solutions that

00:13:45.810 --> 00:13:48.540
really make it now possible to come.

00:13:49.790 --> 00:13:53.770
at reasonable heat development and
reasonable cost, so we can really

00:13:53.800 --> 00:13:57.220
enable these phased array antennas
now also for satellite missions.

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Hywel: Fantastic.

00:13:58.050 --> 00:13:58.200
Yeah.

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Thanks for addressing those the
balance that needs to be struck.

00:14:01.650 --> 00:14:06.130
The heat generation is one thing,
but as we're seeing Something

00:14:06.130 --> 00:14:09.580
of a trend towards larger form
factor systems in the industry.

00:14:09.640 --> 00:14:13.100
This is partially mitigated because
obviously larger systems are able

00:14:13.100 --> 00:14:16.460
to deal with heat generation,
waste heat in different ways.

00:14:16.970 --> 00:14:21.390
And also then you can cope with
more complex engineering, sometimes

00:14:21.390 --> 00:14:22.730
more easily in a larger system.

00:14:23.160 --> 00:14:26.830
Excuse me, but yeah, the balance
that needs to be struck in terms of

00:14:26.890 --> 00:14:28.680
increasing the SWOT budget is key.

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And I, as you highlighted, Michael, the.

00:14:31.795 --> 00:14:36.845
the aim is to get a great balance of
cost for performance, not absolute cost.

00:14:36.855 --> 00:14:42.045
So yeah, if you're, if the cost at
which you're developing data creating,

00:14:42.054 --> 00:14:46.915
generating data, sorry, is lower, and the
data quality is higher based on the same

00:14:46.925 --> 00:14:48.305
unit, then you're in a good position.

00:14:48.315 --> 00:14:52.195
But you also highlighted the complexity
involved in the engineering here.

00:14:52.745 --> 00:14:57.575
As a provider of these sort of systems,
how does Texas Instruments help engineers

00:14:57.575 --> 00:15:01.965
or how can you help engineers to deal
with this complexity and incorporate

00:15:02.565 --> 00:15:06.385
phased array antennas into designs
and development of space missions?

00:15:06.845 --> 00:15:11.465
Adrien: Yeah, so we are really
offering a wide range of solutions

00:15:11.465 --> 00:15:16.005
here to help engineers to, to use
this technology in their designs.

00:15:16.515 --> 00:15:18.395
Let me talk about some of them.

00:15:18.635 --> 00:15:25.295
Obviously we need to start with high speed
ADCs, DACs and analog frontends, right?

00:15:25.635 --> 00:15:31.174
And TI is offering really advanced
ADCs and DACs with high data rates and

00:15:31.184 --> 00:15:36.044
wide bandwidths at the same time with
lower power consumption, lower noise.

00:15:37.264 --> 00:15:42.084
You need those data converters
for capturing and transmitting.

00:15:42.729 --> 00:15:45.759
And to be honest, sometimes
even for processing the high

00:15:45.769 --> 00:15:47.379
frequency signals accurately.

00:15:47.979 --> 00:15:54.779
And I'm thinking here about devices
like the ADC12DJ5200 SP for receiving a

00:15:54.819 --> 00:16:01.539
part, but also on the transmit part, for
example, the DAC39RF10 SP can be used.

00:16:02.719 --> 00:16:07.299
Now, if the customers prefer
more integrated solution.

00:16:07.674 --> 00:16:10.574
We can also offer so
called analog front ends.

00:16:10.614 --> 00:16:16.014
Those products simply integrate several
of those ADCs and DACs into one device.

00:16:16.874 --> 00:16:22.494
And I'm thinking here especially about
the recently released AFE7950 SP.

00:16:22.994 --> 00:16:27.534
Which is our direct sampling
analog front end, which supports

00:16:27.544 --> 00:16:29.094
frequencies up to X band.

00:16:30.794 --> 00:16:35.424
Now, if you talk about ADCs and DACs,
obviously you also need to consider

00:16:35.454 --> 00:16:40.154
clocking, which is also essential for
those kinds of applications because you

00:16:40.164 --> 00:16:42.994
need extremely low phase noise and jitter.

00:16:43.489 --> 00:16:46.439
sometimes even to
femtoseconds level, right?

00:16:47.009 --> 00:16:51.239
And another important topic when
we're talking about clocking is

00:16:51.239 --> 00:16:55.839
the synchronization feature with
very high accuracy sometimes

00:16:55.839 --> 00:16:57.329
down to one picoseconds.

00:16:57.669 --> 00:16:59.289
And this is really essential.

00:16:59.449 --> 00:17:05.729
For maintaining this precise timing
between phased array systems and elements.

00:17:06.239 --> 00:17:10.179
And now if the customers needs a
jitter cleaning and distribution

00:17:10.179 --> 00:17:16.734
capabilities for clocking signals,
they can use our LMK 04832 SP.

00:17:17.124 --> 00:17:21.894
Or if they, for example, need to generate
a signal and need the synthesizer, they

00:17:21.894 --> 00:17:28.594
can use LMX2615 SP or the LMX2694 SP.

00:17:30.614 --> 00:17:36.564
In addition to that, I also wanted
to mention a pretty new trend also

00:17:36.574 --> 00:17:41.454
in space application, a lot of
customers already trying to replace

00:17:41.464 --> 00:17:46.854
their bulky discreet balloons with
fully differential amplifiers.

00:17:47.524 --> 00:17:53.429
And exactly for that reason, We are
offering products with high linearity

00:17:53.429 --> 00:17:59.499
across a wide bandwidth up to 12 gigahertz
at the moment and the current portfolio

00:17:59.499 --> 00:18:05.059
supports one db gain flatness up to
around eight gigahertz at the moment.

00:18:05.909 --> 00:18:11.449
The product is called TRF0206SP
which is exactly four differential

00:18:11.479 --> 00:18:14.189
amplifiers for this kind of application.

00:18:15.369 --> 00:18:19.949
And now the big advantage, this fully
differential amplifier compared to the

00:18:19.959 --> 00:18:23.319
balloon is much smaller and much lighter.

00:18:23.919 --> 00:18:29.739
So that's a really perfect fit for those
space constraints applications like

00:18:29.799 --> 00:18:31.739
communication equipment, for example.

00:18:32.939 --> 00:18:33.289
Hywel: Okay.

00:18:33.289 --> 00:18:33.559
Okay.

00:18:33.559 --> 00:18:33.749
Yeah.

00:18:34.519 --> 00:18:34.699
Yeah.

00:18:34.699 --> 00:18:39.889
I see guys are clearly thinking about
everything required to really incorporate

00:18:40.569 --> 00:18:42.859
the phase array antenna technology into.

00:18:43.714 --> 00:18:48.574
Space mission designs and deal with
the the interfaces and the data rates,

00:18:48.644 --> 00:18:52.354
the managing the data rates and getting
the best out of those systems and

00:18:52.404 --> 00:18:53.954
your communication system as a whole.

00:18:54.134 --> 00:18:57.664
What about the power management,
however how is this dealt with?

00:18:58.134 --> 00:19:01.414
Michael: Yeah, this is of course,
also a super important topic,

00:19:01.414 --> 00:19:03.114
especially on face the ray antenna.

00:19:03.654 --> 00:19:07.244
And the one thing is you
need to have these power.

00:19:07.714 --> 00:19:13.414
Our distribution of power
generation devices a daily, highly

00:19:13.414 --> 00:19:15.144
efficient in a small form factor.

00:19:15.144 --> 00:19:19.784
So we talk about our power
density, very high, and we're

00:19:19.784 --> 00:19:22.754
talking RF signal, RF solutions.

00:19:23.044 --> 00:19:25.394
So we need to also have
very low noise, right?

00:19:25.714 --> 00:19:30.684
We're highly interested in the signal
performance, cannot use any noise there.

00:19:31.354 --> 00:19:32.804
And so there is a.

00:19:33.099 --> 00:19:36.649
Quite a lot of solutions we can offer
here to really provide here a very

00:19:36.669 --> 00:19:38.479
accurate and stable power supply.

00:19:38.929 --> 00:19:44.029
So here's the so called point of
loads, the POLs, like the TPS7H4011

00:19:44.149 --> 00:19:50.139
SP that allows you even up to a 12
volt input to generate They're low

00:19:50.139 --> 00:19:55.889
voltages or you have Another good
example is an LDOA very low noise.

00:19:55.889 --> 00:19:59.339
LDO is called the TPS seven H 1 1 1 1.

00:19:59.909 --> 00:20:08.779
sp very easy to remember that has such low
noise or high PSRR power supply rejection

00:20:08.779 --> 00:20:12.379
ratio is so extremely good on that one
that customers call it really, it's like

00:20:12.379 --> 00:20:17.419
this is an ideal power supply for us and
that is of course, extremely helpful.

00:20:18.029 --> 00:20:21.249
For the end product, of course,
but also during development, as you

00:20:21.249 --> 00:20:25.189
optimize the system, you just know
there's one thing less to worry about,

00:20:25.189 --> 00:20:28.729
you have a perfect rail, whatever
causes your signal to degrade.

00:20:29.079 --> 00:20:32.909
It's not that power rail that makes
things a lot easier for you, of course.

00:20:33.459 --> 00:20:39.129
So that's the overall power tree for
supplying the data converters and maybe

00:20:39.129 --> 00:20:41.579
the FPGA and processing capabilities.

00:20:41.959 --> 00:20:42.639
Another.

00:20:43.039 --> 00:20:47.919
Key element in the power budget is, of
course, the power amplifier, the power

00:20:47.949 --> 00:20:54.109
you transmit has to be all generated
by this power amplifier and these

00:20:54.129 --> 00:20:57.994
solid state power amplifiers, modern
devices, they need a very powerful

00:20:58.884 --> 00:21:01.904
are complex biasing control systems.

00:21:01.904 --> 00:21:05.324
So they need a certain voltage
level that needs to be supplied.

00:21:05.784 --> 00:21:09.844
And according to the temperature
and the current running through

00:21:09.844 --> 00:21:14.524
the power amplifier, you need
to adjust this biasing voltage.

00:21:14.994 --> 00:21:20.209
And Here comes a device from TI
that can, it's really helpful here.

00:21:20.209 --> 00:21:27.309
It's called an AFE11612 SEP, a highly
integrated analog front end that has

00:21:27.309 --> 00:21:34.709
12 DACs and 16 ADCs plus temperature
sensors and a couple of GPIOs integrated.

00:21:35.139 --> 00:21:39.049
And that really helps to get
you the PA biasing and control.

00:21:40.369 --> 00:21:42.079
implemented in a very effective way.

00:21:44.179 --> 00:21:46.399
That's the aspect of
the power tree itself.

00:21:46.399 --> 00:21:50.779
But in space, we have also the topic
and this was many times not really

00:21:51.179 --> 00:21:55.539
immediately thought about is the fault
detection, isolation and recovery.

00:21:55.539 --> 00:21:59.429
So whatever we do in space, we need
to make sure if something goes wrong.

00:21:59.889 --> 00:22:04.939
the electronics quickly identify the
problem, but not only identify it,

00:22:04.939 --> 00:22:08.739
but they need to isolate the problem
from the rest of the system and

00:22:08.739 --> 00:22:13.559
need to see how to recover from that
and get the system back up working.

00:22:13.949 --> 00:22:16.559
So that's fault detection,
isolation, and recovery.

00:22:17.029 --> 00:22:21.099
It's a play of where you need
to, of course, need sensors

00:22:21.449 --> 00:22:22.729
and detect the problem.

00:22:22.729 --> 00:22:27.319
So we have this in our power devices,
oftentimes integrated with the overcurrent

00:22:27.369 --> 00:22:32.269
protection, overvoltage protection and
detection, overtemperature detection

00:22:32.689 --> 00:22:35.479
and corresponding fault output pin.

00:22:35.859 --> 00:22:39.259
So the system can be informed
that something went wrong.

00:22:40.259 --> 00:22:46.509
As we talk about isolation, we have load
switches with even with precision current

00:22:46.509 --> 00:22:52.759
sensing implemented meanwhile, like
here's a device like the TPS7H2140 SP,

00:22:53.589 --> 00:22:57.004
so this is a 32 volt Quad channel issues.

00:22:58.184 --> 00:23:02.544
And these load switches can then
either automatically detect that

00:23:02.544 --> 00:23:07.204
something is wrong and switch off
and isolate the problematic system

00:23:07.244 --> 00:23:12.134
from the rest of the bus, or can be
actually be controlled by another

00:23:12.724 --> 00:23:16.244
system manager to disconnect things.

00:23:16.674 --> 00:23:20.644
And this control and management
or orchestrating this whole fault

00:23:20.664 --> 00:23:25.004
detection, isolation and recovery
There comes a device handy.

00:23:25.234 --> 00:23:25.854
It's called the

00:23:29.434 --> 00:23:30.234
TMS570LC4357 SEP.

00:23:30.464 --> 00:23:33.564
It's an MCU we just
released for SpaceGrade.

00:23:33.974 --> 00:23:40.464
It's a device integrating our Cortex
R5 floating point cores and actually

00:23:40.504 --> 00:23:43.094
two of them are operating in lockstep.

00:23:43.794 --> 00:23:49.539
And this overall design here being
especially developed for high reliability

00:23:49.539 --> 00:23:54.119
applications that offers a really a
very high diagnostic coverage, but also

00:23:54.129 --> 00:23:59.219
a very near instant fault detection,
as we call it, and it's here very

00:23:59.219 --> 00:24:01.679
helpful in orchestrate the FDIR.

00:24:04.909 --> 00:24:08.454
Adrien: Michael, let me, At maybe
additional point also on the

00:24:08.464 --> 00:24:10.304
multi mission support, right?

00:24:10.544 --> 00:24:15.004
Because it's also a very important
point and TI supports simply

00:24:15.004 --> 00:24:17.104
different mission requirements also.

00:24:17.104 --> 00:24:23.314
So depending on the orbit customer
is operating the application, so low

00:24:23.374 --> 00:24:29.314
earth orbit or geostationary orbit The
customers can choose between a plastic

00:24:29.364 --> 00:24:36.304
package with higher radiation performance,
so called QML class P, or plastic

00:24:36.304 --> 00:24:39.454
space enhanced product, so called SEP.

00:24:40.084 --> 00:24:44.434
And now the most important
advantage, those products are in

00:24:44.434 --> 00:24:50.104
most cases pin to pin compatible,
which offers a huge flexibility

00:24:50.104 --> 00:24:52.084
for customers in their designs.

00:24:52.444 --> 00:24:57.994
And at the same time, it makes
Sure, customers are using dedicated

00:24:58.024 --> 00:25:00.824
product for their space environment.

00:25:01.389 --> 00:25:01.889
Okay.

00:25:01.989 --> 00:25:05.489
Hywel: Yeah, this is a very important
aspect as well, as we're seeing as

00:25:05.489 --> 00:25:10.019
we discussed, more versatile missions
longer missions or missions with multiple

00:25:10.019 --> 00:25:15.359
goals that may be in different orbits
potentially or a customer who's creating

00:25:15.359 --> 00:25:19.559
technology for different, different
satellites or different vehicles, whatever

00:25:19.559 --> 00:25:25.579
it is for different orbits that, but they
want to, limit non recurring energy by

00:25:25.679 --> 00:25:30.659
non recurring engineering, apologies, with
a consistent aspect of the technology.

00:25:30.679 --> 00:25:31.829
So yeah, this is great.

00:25:31.839 --> 00:25:32.169
Thank you.

00:25:32.169 --> 00:25:36.499
So I can see how much that TI is
doing in this area and mentioning

00:25:36.529 --> 00:25:40.159
fault detection and understand the
power management separately from

00:25:40.209 --> 00:25:42.679
the data data rates and the data.

00:25:43.509 --> 00:25:46.899
chain compatibility
has been really useful.

00:25:46.899 --> 00:25:47.369
Thank you.

00:25:47.439 --> 00:25:50.719
Thank you for going into detail on this
and to the listeners, we'll obviously

00:25:50.719 --> 00:25:54.969
share more information about the
different products and TI resources that

00:25:54.969 --> 00:25:56.559
have been mentioned in the show notes.

00:25:56.569 --> 00:26:01.759
So you can read more into how these
sorts of technologies and the designs

00:26:01.759 --> 00:26:05.889
of the application notes and the
thinking behind them can be readily

00:26:05.889 --> 00:26:09.719
incorporated into your designs, your
plans if this is of interest to you.

00:26:09.719 --> 00:26:11.169
So thank you guys for that.

00:26:12.059 --> 00:26:18.159
I just wanted to wrap up by, yeah, coming
back to the topic that we started with and

00:26:18.449 --> 00:26:24.179
discuss how in a wider sense, you see this
aspect of the space industry evolving.

00:26:24.519 --> 00:26:27.789
It would seem like the RF
spectrum is only going to become

00:26:27.899 --> 00:26:29.239
more crowded in the short term.

00:26:29.789 --> 00:26:35.189
And We might then run into issues with
an increased regulatory burden, where

00:26:35.189 --> 00:26:39.679
the bodies in charge of apportioning
and controlling the spectrum are

00:26:39.679 --> 00:26:44.529
requiring a greater, admin overhead of
space missions and companies might even

00:26:44.539 --> 00:26:47.329
make it difficult for some companies,
especially those smaller, newer

00:26:47.329 --> 00:26:49.459
teams to get satellites into orbit.

00:26:49.954 --> 00:26:53.624
On the timescales and budgets
that, that makes sense to them.

00:26:53.674 --> 00:26:57.614
Yeah, I wondered what your thoughts
were on how you see this area changing

00:26:57.614 --> 00:26:59.944
and progressing, moving forwards.

00:27:00.444 --> 00:27:00.914
Yeah, I

00:27:01.164 --> 00:27:04.804
Michael: think it's definitely on
the move and I think we have reached.

00:27:05.204 --> 00:27:06.034
Critical mass.

00:27:06.034 --> 00:27:10.704
So that's the trend to face Dorian tennis
is probably very hard to reverse anymore.

00:27:11.074 --> 00:27:14.244
But what we will definitely see
moving forward is that we will see

00:27:14.244 --> 00:27:16.254
an increase of number of elements.

00:27:16.754 --> 00:27:20.424
Because that gives you always, as we
talked about before, a more focused

00:27:20.434 --> 00:27:25.304
beam that you want and allows you
also have even more beams per antenna.

00:27:25.654 --> 00:27:29.464
And that all translates then into
those benefits of you have maybe

00:27:29.814 --> 00:27:35.854
more users and higher data rates per
user per beam, more users overall.

00:27:35.854 --> 00:27:38.204
So just a bigger business after all.

00:27:38.214 --> 00:27:43.084
The other trend, as you say, the
spectrum is getting crowded, so people

00:27:43.294 --> 00:27:47.854
try to go even higher frequency bands
and as technology proceeds where

00:27:47.854 --> 00:27:52.104
this is entirely possible, and here
comes for change something good.

00:27:52.174 --> 00:27:57.184
The higher you go in frequency
you're shrinking the space needed

00:27:57.204 --> 00:27:58.704
between the antenna elements.

00:27:59.054 --> 00:27:59.834
So this is you.

00:28:00.264 --> 00:28:01.774
How you put them together.

00:28:02.074 --> 00:28:07.034
Then if these spaces go even smaller,
you can have put more elements

00:28:07.534 --> 00:28:11.434
per antenna, per square meter
or per area if you want, right?

00:28:11.704 --> 00:28:14.424
So that's actually going
really the right direction.

00:28:14.824 --> 00:28:17.084
What's not helping here
is that your heat problem.

00:28:17.409 --> 00:28:19.279
increases the moment, right?

00:28:19.279 --> 00:28:23.919
You put even more electronics on an
even denser space, but that is where

00:28:24.139 --> 00:28:29.669
yeah, or companies like us at Texas
will keep working to help on that area.

00:28:30.429 --> 00:28:33.699
Another positive trend in the
satellite technology is that the

00:28:33.699 --> 00:28:36.649
cost of launch per the kilogram.

00:28:37.269 --> 00:28:39.919
per weight keeps this decreasing.

00:28:40.039 --> 00:28:43.659
So that's just where we have multiple
new players now that help bring down the

00:28:43.659 --> 00:28:45.689
cost in this newer rockets and launches.

00:28:46.149 --> 00:28:50.659
And that enables them even more
satellite players, more application

00:28:50.659 --> 00:28:53.149
services, business models there.

00:28:53.149 --> 00:28:56.229
And maybe look at an
example like cell phones.

00:28:56.239 --> 00:29:00.099
Of course, they're directly connected
to satellites already today.

00:29:00.369 --> 00:29:05.129
We can do voice, we can do text, but
moving forward, we will have true

00:29:05.219 --> 00:29:10.929
broadband Our internet access over
satellites from our cell phones.

00:29:11.909 --> 00:29:16.959
So in every area of the, on earth, you can
really reach your broadband connectivity.

00:29:17.759 --> 00:29:23.829
And so we see there is an
continuous grow and development

00:29:23.849 --> 00:29:25.519
in this market ahead of us.

00:29:26.069 --> 00:29:30.159
That means that our customers need
to redevelop, but they also want

00:29:30.159 --> 00:29:32.586
to reuse things they want to, use.

00:29:32.956 --> 00:29:36.766
Standardized components, so they don't
always have to start from scratch.

00:29:36.976 --> 00:29:40.526
They can really have an evolution
in the product development.

00:29:41.086 --> 00:29:45.076
And there's also the need for
one development and support

00:29:45.106 --> 00:29:46.586
multiple mission profiles.

00:29:47.226 --> 00:29:51.926
Adrian had pointed out you have
the SEP for the LEO missions,

00:29:51.966 --> 00:29:53.996
the QMLP for the GEO missions.

00:29:54.606 --> 00:29:56.916
Moving forward, you have
the pin compatibility.

00:29:57.636 --> 00:30:02.376
And all that in mind this is where TI is
so convinced what's needed here is really.

00:30:02.736 --> 00:30:07.346
Space great catalog products in a way,
you know what they are, you can reorder

00:30:08.116 --> 00:30:12.476
when you want them, you can reorder
as many as you want, and you can do

00:30:12.476 --> 00:30:14.996
this also in 10 or 15 years from now.

00:30:15.476 --> 00:30:16.116
Hywel: Fantastic.

00:30:16.616 --> 00:30:20.096
That makes sense as the, as a,
an approach to the industry.

00:30:20.106 --> 00:30:23.556
Yeah, I think we've seen how this.

00:30:23.926 --> 00:30:26.746
These kinds of approaches obviously
work in other industry sectors.

00:30:26.746 --> 00:30:30.296
And I think yeah, TI is really doing
a great job of operating in this

00:30:30.296 --> 00:30:34.896
manner and yeah, it was great to
to understand your thinking behind

00:30:35.026 --> 00:30:36.666
how this area is moving forward.

00:30:36.666 --> 00:30:40.016
So I think this is a great place
to wrap up today's conversation.

00:30:40.046 --> 00:30:41.246
Thank you both for sharing.

00:30:41.326 --> 00:30:45.506
Thank you, Adrian and Michael for sharing
so many of your insights today on how.

00:30:45.851 --> 00:30:50.001
Face array antennas work what
they use for the advantages that

00:30:50.001 --> 00:30:51.561
they bring, how to cope with.

00:30:52.246 --> 00:30:56.156
The trade offs in terms of, the power
and the heat and the engineering

00:30:56.236 --> 00:31:02.566
complexity and what can be done to ease
that integration and of the, of such

00:31:02.706 --> 00:31:06.296
technologies into existing designs and
space missions and plans for the future.

00:31:06.296 --> 00:31:08.056
So thank you both very much.

00:31:08.106 --> 00:31:10.786
We'll share, and to the listeners,
we'll share more information on the

00:31:10.786 --> 00:31:14.556
products and resources mentioned by
the guests today in the show notes.

00:31:15.066 --> 00:31:15.836
And you can find out.

00:31:16.586 --> 00:31:20.516
More about TI on their website and on
their search portfolio, which is very

00:31:20.516 --> 00:31:24.306
extensive and has a lot of information on
the products that we've discussed today.

00:31:24.946 --> 00:31:28.266
So thank you to everybody out there
for spending time with us today

00:31:28.266 --> 00:31:29.626
on the Space Industry Podcast.

00:31:29.626 --> 00:31:31.436
We really appreciate your attention.

00:31:31.686 --> 00:31:36.596
If you like the show, please give
us an honest rating and review

00:31:36.596 --> 00:31:38.056
on your favorite podcast player.

00:31:38.521 --> 00:31:42.711
And stay tuned for the next episode of the
show, when we will be speaking to more of

00:31:42.711 --> 00:31:44.921
the companies taking us all into orbit.

00:31:45.311 --> 00:31:46.071
Thank you very much.

00:31:48.831 --> 00:31:52.351
Thank you for listening to this episode
of the Space Industry by SatSearch.

00:31:52.701 --> 00:31:55.871
I hope you enjoyed today's story about
one of the companies taking us into orbit.

00:31:56.491 --> 00:31:58.971
We'll be back soon with more in
depth, behind the scenes insights

00:31:58.981 --> 00:32:00.301
from private space businesses.

00:32:00.871 --> 00:32:02.741
In the meantime, you can go to satsearch.

00:32:02.751 --> 00:32:06.761
com for more information on the space
industry today, or find us on social media

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