Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Fabiano Moser
Hi,

AMSAT can open a Project at KICKSTARTER in technology tag.
https://www.kickstarter.com/discover/categories/technology

I saw a lot of project getting 300, 400% more than originally goal. Some of
then looks like a stupid idea, but that´s no matter they get the found´s,
and what make no sense for me can be a good deal to others :)

Already donated via PAYPAL today, but in my opinion would be great if
AMSAT-NA use this way also to get founds for the project!

Please think about it, I believe that donations don´t need to come only
from amateur radio satellite operators, but also from everyone who likes
electronics, science and technology.

73
Fabiano Moser
CT7ABD
PY5RX



On Sat, Jul 19, 2014 at 10:50 PM, Phil Karn k...@ka9q.net wrote:

 On 07/19/2014 02:04 PM, Jerry Buxton wrote:

  other three would be ready to fly if other opportunities came up.  If
  you're going to spend the time developing them, why not partner for free
  launches (ELaNa) for more than one?  The opportunities for an FM
  transponder and educational outreach are good.  I still have
  universities looking to partner.

 Ah, because launches are scarce and expensive, and (re)developing even
 the same old thing consumes much of AMSAT's limited resources. And
 they're limited because we have yet to interest more than a tiny niche
 in what we're doing.

 It's great to have universities looking to partner, but what do they
 bring to the table, really? Are we sure they're not just looking for
 free spectrum?

  one flying soon, so that we can learn how well they work and apply those
  lessons to Fox-2 while we're working out the design.

 We already know how well they'll work because we've done the same thing
 many times before. I hate to say it, but this is no longer rocket
 science. The physics is well understood, and those same physics tell us
 how we could accomplish so much more with our (currently) limited
 resources.

 --Phil

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Phil Karn
On 07/19/2014 09:23 PM, Robert Bruninga wrote:

 I cannot believe that.  The equilibrium of a nominally black (solar panels
 on all sides) spacecraft is something like about 0 to 30 C (32F to 90F) a
 very benign operational range.  The only time you DO have thermal issues is
 when you DO have attitude control and have things that are not equally over
 time seeing the sun and dark sky.

See Dick's paper for the details; I'm just quoting his results. I know
the basic physics of heat transfer in space but I would never call
myself an expert. He is.

But I can do a back-of-the-envelope calculation that tells me he's right.

The solar cells they're using have an absorptivity and emissivity that
is both 0.98, as I recall, so a cubesat covered with them is essentially
a perfect blackbody.

A blackbody cube with one face normal to the sun at 1 AU will reach an
equilibrium temperature of -21.35 C. The problem is that the ratio of
radiating area to absorbing area for a cube is 6:1 (with the sun normal
to one surface). A sphere would be warmer because its ratio of radiating
to absorbing area is only 4:1. A thin flat plate normal to the sun (like
a solar wing) would be even warmer -- 2:1.

And that -21.35 C figure is for continuous sunlight. Throw in eclipses
and things get much worse. Yes, it would be a little better when the sun
shines on a corner rather than normal to a face, and Earth albedo and IR
radiation will warm things a little, but not enough to matter.

--Phil

PS: Temperature of 10 cm blackbody cube at 1 AU:

Area facing sun: .01 m^2
Solar constant: 1367.5 W/m^2
Absorbed power = 13.675 W

Total radiating area: .06 m^2
Emissivity = 1.0 (perfect blackbody)
Stefan-Boltzmann constant = 5.6703e-8 W/(m^2K^4)


T = (13.675 W / (5.6703e-8 * 1.0 * .06)) ** (1/4)
  = 251.8K == -21.35 C
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Wouter Weggelaar
Hi All,

I could start writing all kinds of angry E-mails, but I have always
resisted to reply on these kind of threads.

I'm glad the AMSAT-BB is not reflecting the great community that is amateur
radio and the many exciting things we are doing for our community to keep
communications alive.

I will go back to work on SDR transponders, D-ATV cubesats, CODEC2 speech
downlinks and FUNcube linear transponder improvements, but you guys are not
interested I hear, so I will shut up.


Wouter PA3WEG





On Sun, Jul 20, 2014 at 12:59 PM, Phil Karn k...@ka9q.net wrote:

 On 07/19/2014 09:23 PM, Robert Bruninga wrote:

  I cannot believe that.  The equilibrium of a nominally black (solar
 panels
  on all sides) spacecraft is something like about 0 to 30 C (32F to 90F) a
  very benign operational range.  The only time you DO have thermal issues
 is
  when you DO have attitude control and have things that are not equally
 over
  time seeing the sun and dark sky.

 See Dick's paper for the details; I'm just quoting his results. I know
 the basic physics of heat transfer in space but I would never call
 myself an expert. He is.

 But I can do a back-of-the-envelope calculation that tells me he's right.

 The solar cells they're using have an absorptivity and emissivity that
 is both 0.98, as I recall, so a cubesat covered with them is essentially
 a perfect blackbody.

 A blackbody cube with one face normal to the sun at 1 AU will reach an
 equilibrium temperature of -21.35 C. The problem is that the ratio of
 radiating area to absorbing area for a cube is 6:1 (with the sun normal
 to one surface). A sphere would be warmer because its ratio of radiating
 to absorbing area is only 4:1. A thin flat plate normal to the sun (like
 a solar wing) would be even warmer -- 2:1.

 And that -21.35 C figure is for continuous sunlight. Throw in eclipses
 and things get much worse. Yes, it would be a little better when the sun
 shines on a corner rather than normal to a face, and Earth albedo and IR
 radiation will warm things a little, but not enough to matter.

 --Phil

 PS: Temperature of 10 cm blackbody cube at 1 AU:

 Area facing sun: .01 m^2
 Solar constant: 1367.5 W/m^2
 Absorbed power = 13.675 W

 Total radiating area: .06 m^2
 Emissivity = 1.0 (perfect blackbody)
 Stefan-Boltzmann constant = 5.6703e-8 W/(m^2K^4)


 T = (13.675 W / (5.6703e-8 * 1.0 * .06)) ** (1/4)
   = 251.8K == -21.35 C
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Rick Walter
I was not going to post but since no one else has, I thought there needs to be 
a correction to a statement made in case some younger people are reading the 
thread. 

Phil said:
Good analogy, actually. They returned to the moon six times (succeeding
on five) because they had excess hardware originally built in the
expectation that the first attempts would fail.

There were actually seven manned missions to the moon. Six succeeded. Apollo 13 
never landed on the moon and returned to earth safely. Apollo 11,12,14,15,16, 
and 17 landed. 12 American astronauts walked on the moon. 

Sent from Rick's iPad2

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Rick Walter
I need to receive the foot in mouth award. The key word I read past was They 
RETURNED to the moon six... I'll just go back to the my radios and hide.

Sent from Rick's iPad2

 On Jul 20, 2014, at 9:27 AM, Rick Walter wb3...@gmail.com wrote:
 
 I was not going to post but since no one else has, I thought there needs to 
 be a correction to a statement made in case some younger people are reading 
 the thread. 
 
 Phil said:
 Good analogy, actually. They returned to the moon six times (succeeding
 on five) because they had excess hardware originally built in the
 expectation that the first attempts would fail.
 
 There were actually seven manned missions to the moon. Six succeeded. Apollo 
 13 never landed on the moon and returned to earth safely. Apollo 
 11,12,14,15,16, and 17 landed. 12 American astronauts walked on the moon. 
 
 Sent from Rick's iPad2
 
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread g0mrf

I must quickly point out some real data:
 
www.warehouse.funcube.org.uk
 
Which shows an equilibrium of around +20 degrees after 64 minutes of sunlight.
Black solar cells on a black surface but some polished Aluminium in the 
structure.
 
During eclipse, The Earth facing side begins to increase in temperature at 
around -16 degrees, but then cools down rapidly as the cube rotates. The 
temperature is still heading down rapidly as it exits eclipse after 34 minutes 
and at around -24C on the outside surfaces.
 
Thanks
 
David
 
 
-Original Message-
From: Phil Karn k...@ka9q.net
To: amsat-bb amsat-bb@amsat.org
Sent: Sun, 20 Jul 2014 11:59
Subject: Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT 
Fox-1C Launch Opportunity Announced


On 07/19/2014 09:23 PM, Robert Bruninga wrote:

 I cannot believe that.  The equilibrium of a nominally black (solar panels
 on all sides) spacecraft is something like about 0 to 30 C (32F to 90F) a
 very benign operational range.  The only time you DO have thermal issues is
 when you DO have attitude control and have things that are not equally over
 time seeing the sun and dark sky.

See Dick's paper for the details; I'm just quoting his results. I know
the basic physics of heat transfer in space but I would never call
myself an expert. He is.

But I can do a back-of-the-envelope calculation that tells me he's right.

The solar cells they're using have an absorptivity and emissivity that
is both 0.98, as I recall, so a cubesat covered with them is essentially
a perfect blackbody.

A blackbody cube with one face normal to the sun at 1 AU will reach an
equilibrium temperature of -21.35 C. The problem is that the ratio of
radiating area to absorbing area for a cube is 6:1 (with the sun normal
to one surface). A sphere would be warmer because its ratio of radiating
to absorbing area is only 4:1. A thin flat plate normal to the sun (like
a solar wing) would be even warmer -- 2:1.

And that -21.35 C figure is for continuous sunlight. Throw in eclipses
and things get much worse. Yes, it would be a little better when the sun
shines on a corner rather than normal to a face, and Earth albedo and IR
radiation will warm things a little, but not enough to matter.

--Phil

PS: Temperature of 10 cm blackbody cube at 1 AU:

Area facing sun: .01 m^2
Solar constant: 1367.5 W/m^2
Absorbed power = 13.675 W

Total radiating area: .06 m^2
Emissivity = 1.0 (perfect blackbody)
Stefan-Boltzmann constant = 5.6703e-8 W/(m^2K^4)


T = (13.675 W / (5.6703e-8 * 1.0 * .06)) ** (1/4)
  = 251.8K == -21.35 C
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Graham Shirville

Hi Phil,

The reality is, even with no battery heater on FUNcube-1 we seem to have an 
acceptable battery temperature of between 0 and +5C. The temp sensor is, of 
course, actually external to the battery itself.


Our orbit is sun synchronous so we suffer eclipses for approx 33% of the 
orbit ..but then we are relatively close to the earth!


I would also comment that any active attitude control system will consume 
power...which we don't have much of..


Probably, if you need continuous operation of the radio system, then a 2U 
with deployable solar panels is the minimum configuration for a CubeSat 
operating on microwave bands with an active attitude control system.


best 73

Graham
G3VZV


-Original Message- 
From: g0...@aol.com

Sent: Sunday, July 20, 2014 3:41 PM
To: k...@ka9q.net ; amsat-bb@amsat.org ; bruni...@usna.edu
Subject: Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT 
Fox-1C Launch Opportunity Announced



I must quickly point out some real data:

www.warehouse.funcube.org.uk

Which shows an equilibrium of around +20 degrees after 64 minutes of 
sunlight.
Black solar cells on a black surface but some polished Aluminium in the 
structure.


During eclipse, The Earth facing side begins to increase in temperature at 
around -16 degrees, but then cools down rapidly as the cube rotates. The 
temperature is still heading down rapidly as it exits eclipse after 34 
minutes and at around -24C on the outside surfaces.


Thanks

David


-Original Message-
From: Phil Karn k...@ka9q.net
To: amsat-bb amsat-bb@amsat.org
Sent: Sun, 20 Jul 2014 11:59
Subject: Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT 
Fox-1C Launch Opportunity Announced



On 07/19/2014 09:23 PM, Robert Bruninga wrote:


I cannot believe that.  The equilibrium of a nominally black (solar panels
on all sides) spacecraft is something like about 0 to 30 C (32F to 90F) a
very benign operational range.  The only time you DO have thermal issues 
is
when you DO have attitude control and have things that are not equally 
over

time seeing the sun and dark sky.


See Dick's paper for the details; I'm just quoting his results. I know
the basic physics of heat transfer in space but I would never call
myself an expert. He is.

But I can do a back-of-the-envelope calculation that tells me he's right.

The solar cells they're using have an absorptivity and emissivity that
is both 0.98, as I recall, so a cubesat covered with them is essentially
a perfect blackbody.

A blackbody cube with one face normal to the sun at 1 AU will reach an
equilibrium temperature of -21.35 C. The problem is that the ratio of
radiating area to absorbing area for a cube is 6:1 (with the sun normal
to one surface). A sphere would be warmer because its ratio of radiating
to absorbing area is only 4:1. A thin flat plate normal to the sun (like
a solar wing) would be even warmer -- 2:1.

And that -21.35 C figure is for continuous sunlight. Throw in eclipses
and things get much worse. Yes, it would be a little better when the sun
shines on a corner rather than normal to a face, and Earth albedo and IR
radiation will warm things a little, but not enough to matter.

--Phil

PS: Temperature of 10 cm blackbody cube at 1 AU:

Area facing sun: .01 m^2
Solar constant: 1367.5 W/m^2
Absorbed power = 13.675 W

Total radiating area: .06 m^2
Emissivity = 1.0 (perfect blackbody)
Stefan-Boltzmann constant = 5.6703e-8 W/(m^2K^4)


T = (13.675 W / (5.6703e-8 * 1.0 * .06)) ** (1/4)
 = 251.8K == -21.35 C
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Bob- W7LRD
a different slant-not wanting to enter the fm vs linear ongoing debate or the 
easy sat concept-I started satellites not because it was easy, but because it 
was hard, and at times still is!  This was back in the days of the RS 
satellites.  I believe if you present the challenge they will come.  
Unfortunately we need the money upfront not after the fact.  Perhaps this 
incremental effort toward HEO or MEO is required, however we (AMSAT's) have 
been doing this for a long time and I think should have had our ducks lined 
up by now.   We're a bunch of cleaver people and should develop a method 
getting the necessary funds for launches.  Everything is now bottom line 
driven.  We should just do it.  
73 Bob W7LRD 
Seattle 

- Original Message -

From: Paul Stoetzer n...@arrl.net 
To: Phil Karn k...@ka9q.net 
Cc: amsat-bb@amsat.org 
Sent: Saturday, July 19, 2014 12:28:12 PM 
Subject: Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT 
Fox-1C Launch Opportunity Announced 

Are FM repeater satellites what we all want in orbit? No. Personally, 
I'd like a Mode J linear transponder in a sun synchronous circular 
orbit of about 2,000km (if we can't get anything to HEO). 

However, the Fox-1A, Fox-1B, Fox-1C, and Fox-1D satellites will 
eventually lead to the Fox-2 series of satellites. The software 
designed transponders on board the Fox-2 series will be capable of 
operating in any number of digital communications modes as well as 
operating as linear transponders. 

AO-51's V/U FM repeater was probably the most popular amateur 
satellite ever launched. Since the loss of AO-51, AMSAT-NA membership 
has been declining and is at the point where membership dues alone do 
not sustain the operating costs of the organization. 

Right now, those who are mildly interested in amateur satellites have 
one satellite to try with a minimal investment: SO-50, which is a 
satellite that for about half the days of each month is not convenient 
for most people who work 9-5 and sleep 10-6 and has a weak downlink 
that is often very difficult for newcomers to hear. Even experienced 
satellite operators are at times heard to transmit without being able 
to hear the satellite. With EO-80 (QB50p2), Fox-1A, and Fox-1C 
hopefully in orbit and operational next year, there will be three 
easily heard FM satellites (the 9 dB advantage of the 2m downlinks on 
these satellites will be quite welcome) - two in sun synchronous 
orbits with relatively consistent pass times. Having those satellites 
in orbit will mean that more hams get bitten by the satellite bug, 
join AMSAT, and progress to improving their stations to operate on the 
linear transponders and, potentially, on digital satellites. 

Bottom line - an AMSAT with more satellites in orbit means an AMSAT 
with more members and that's how we are eventually going to get our 
ideal satellites in orbit. 

73, 

Paul, N8HM 

On Sat, Jul 19, 2014 at 2:54 PM, Phil Karn k...@ka9q.net wrote: 
 On 07/18/2014 12:08 PM, Joseph Spier wrote: 
 
 Fox-1C is the third of four Fox-1 series satellites under 
 development, with Fox-1A and RadFXsat/Fox-1B launching through the 
 NASA ELANA program. Fox-1C will carry an FM repeater system for 
 amateur radio for use by radio hams and listeners worldwide. 
 
 YET ANOTHER analog satellite? 
 
 I'm not interested. 
 
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Paul Stoetzer
Getting the $125,000 to launch a 1U cubesat into LEO should be plenty
doable, but raising $10-$15 million for a launch to HEO?

AMSAT-DL has been raising funds for P3E now for nearly a decade. If
they thought they had a chance of success, I'm sure there'd be a much
more public push to raise those funds.

Unfortunately, there are not enough amateur radio operators interested
in the amateur satellite program to put up that kind of money. Million
dollar DXpeditions are doable because of the broad interest among the
amateur radio community in funding those projects. A good number of
amateur radio operators are only vaguely aware of the amateur
satellite program and consider it to be quite esoteric. Heck, on the
extremely rare occasion that the amateur satellite program merits a
mention in a QST column these days, it's often in WB8IMY's Eclectic
Technology column. That, unfortunately, shows you how the amateur
radio community as a whole views the amateur satellite program.

The bottom line is that AMSAT-NA needs a significant boost in
membership and visibility and that boost needs to be soon. Putting two
satellites into orbit that nearly every single ham will be able to
easily hear (even a $30 Baofeng and it's stock duck should hear high
passes of the Fox-1 satellites) along with the accompanying publicity
should provide that boost. ARISSat-1 and the heavy publicity in QST
and other amateur radio news sources is what got me involved in
amateur satellites, though it would take me another two years before I
really got into it seriously. Now I've really been bitten by the bug:
293 grids, 48 states, 4 Canadian provinces, and 27 DXCCs in my log
plus I've done two public demonstrations of amateur satellites and
assisted the AMSAT booth and demo station at Dayton. That's all
because of a project derided by many on this board as a waste of
AMSAT's time and resources!

73,

Paul, N8HM



On Sun, Jul 20, 2014 at 12:42 PM, Bob- W7LRD w7...@comcast.net wrote:
 a different slant-not wanting to enter the fm vs linear ongoing debate or
 the easy sat concept-I started satellites not because it was easy, but
 because it was hard, and at times still is!  This was back in the days of
 the RS satellites.  I believe if you present the challenge they will come.
 Unfortunately we need the money upfront not after the fact.  Perhaps this
 incremental effort toward HEO or MEO is required, however we (AMSAT's)
 have been doing this for a long time and I think should have had our ducks
 lined up by now.   We're a bunch of cleaver people and should develop a
 method getting the necessary funds for launches.  Everything is now bottom
 line driven.  We should just do it.
 73 Bob W7LRD
 Seattle

 
 From: Paul Stoetzer n...@arrl.net

 To: Phil Karn k...@ka9q.net
 Cc: amsat-bb@amsat.org
 Sent: Saturday, July 19, 2014 12:28:12 PM
 Subject: Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT
 Fox-1C Launch Opportunity Announced


 Are FM repeater satellites what we all want in orbit? No. Personally,
 I'd like a Mode J linear transponder in a sun synchronous circular
 orbit of about 2,000km (if we can't get anything to HEO).

 However, the Fox-1A, Fox-1B, Fox-1C, and Fox-1D satellites will
 eventually lead to the Fox-2 series of satellites. The software
 designed transponders on board the Fox-2 series will be capable of
 operating in any number of digital communications modes as well as
 operating as linear transponders.

 AO-51's V/U FM repeater was probably the most popular amateur
 satellite ever launched. Since the loss of AO-51, AMSAT-NA membership
 has been declining and is at the point where membership dues alone do
 not sustain the operating costs of the organization.

 Right now, those who are mildly interested in amateur satellites have
 one satellite to try with a minimal investment: SO-50, which is a
 satellite that for about half the days of each month is not convenient
 for most people who work 9-5 and sleep 10-6 and has a weak downlink
 that is often very difficult for newcomers to hear. Even experienced
 satellite operators are at times heard to transmit without being able
 to hear the satellite. With EO-80 (QB50p2), Fox-1A, and Fox-1C
 hopefully in orbit and operational next year, there will be three
 easily heard FM satellites (the 9 dB advantage of the 2m downlinks on
 these satellites will be quite welcome) - two in sun synchronous
 orbits with relatively consistent pass times. Having those satellites
 in orbit will mean that more hams get bitten by the satellite bug,
 join AMSAT, and progress to improving their stations to operate on the
 linear transponders and, potentially, on digital satellites.

 Bottom line - an AMSAT with more satellites in orbit means an AMSAT
 with more members and that's how we are eventually going to get our
 ideal satellites in orbit.

 73,

 Paul, N8HM

 On Sat, Jul 19, 2014 at 2:54 PM, Phil Karn k...@ka9q.net wrote:
 On 07/18/2014 12:08 PM, Joseph

Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread John Becker


On 7/20/2014 12:00 PM, Paul Stoetzer wrote: IN PART

The bottom line is that AMSAT-NA needs a significant boost in
membership and visibility and that boost needs to be soon.

I gave up on AMSAT when it seemed that the main afford was put into
FM in and FM out satellites. Membership ran out many (15) years ago.

John
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Paul Stoetzer
The Fox-1 series of satellites will lead to the Fox-2 series with many
more interesting modes and capabilities. Yes, the priority is on
building and launching the Fox-1 series, but a good portion of that
work will be done by next year and then the lessons learned can be
applied to constructing and launching the Fox-2 series.

The reality is, of course, that FM satellites are extremely popular. I
have read through much of the AMSAT-BB archives and I find a ton more
posts about grid and country activations from back when AO-51 was
alive than what you see now. Getting on the linear satellites is not
expensive or complicated at all, but for whatever reason, we just have
not been able to communicate that it's both fun, extremely rewarding,
and that won't break the bank doing it to the amateur radio community
as a whole, so for those of us who enjoy chasing grids, states,
provinces, DX, etc, we do rely on the availability of FM satellites to
activate those areas.

Also remember that AMSAT is a membership organization. If members are
not happy with the direction of the organization, they are free to
select directors who prioritize what the membership desires.
Non-members, however, have no voice in the proceedings.

73,

Paul, N8HM

On Sun, Jul 20, 2014 at 1:19 PM, John Becker w0...@big-river.net wrote:

 On 7/20/2014 12:00 PM, Paul Stoetzer wrote: IN PART

 The bottom line is that AMSAT-NA needs a significant boost in
 membership and visibility and that boost needs to be soon.

 I gave up on AMSAT when it seemed that the main afford was put into
 FM in and FM out satellites. Membership ran out many (15) years ago.

 John

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Clayton Coleman
This is great news.

I thank all the AMSAT volunteers, past and present for this opportunity.

GO FOX, GO!

73
Clayton
W5PFG
 On Jul 18, 2014 2:11 PM, Joseph Spier w...@vfr.net wrote:

 AMSAT NEWS SERVICE
 ANS-199

 The AMSAT News Service bulletins are a free, weekly news and infor-
 mation service of AMSAT North America, The Radio Amateur Satellite
 Corporation. ANS publishes news related to Amateur Radio in Space
 including reports on the activities of a worldwide group of Amateur
 Radio operators who share an active interest in designing, building,
 launching and communicating through analog and digital Amateur Radio
 satellites.

 The news feed on http://www.amsat.org publishes news of Amateur
 Radio in Space as soon as our volunteers can post it.

 Please send any amateur satellite news or reports to:
 ans-editor at amsat.org.

 In this edition:

 * AMSAT Fox-1C Launch Opportunity Announced

 SB SAT @ AMSAT $ANS-199.01
 ANS-199 AMSAT News Service Special Bulletin

 AMSAT News Service Bulletin 199.01
 From AMSAT HQ KENSINGTON, MD.
 DATE July 18, 2014
 To All RADIO AMATEURS
 BID: $ANS-199.01


 -


 AMSAT Fox-1C Launch Opportunity Announced


 AMSAT is excited to announce a launch opportunity for the Fox-1C
 Cubesat. AMSAT has teamed with Spaceflight Inc. for integration and
 launch utilizing Spaceflight's SHERPA system to a sun-synchronous
 orbit in the third quarter of 2015.

 Fox-1C is the third of four Fox-1 series satellites under
 development, with Fox-1A and RadFXsat/Fox-1B launching through the
 NASA ELANA program. Fox-1C will carry an FM repeater system for
 amateur radio for use by radio hams and listeners worldwide. Further
 details on the satellite and launch will be made available as soon
 as released.

 AMSAT has an immediate need to raise funds to cover both the launch
 contract and additional materials for construction and testing for
 Fox-1C. We have set a fundraising goal of $125,000 dollars to cover
 these expenses over the next 12 months, and allow us to continue to
 keep amateur radio in space.

 Donations may be made through the AMSAT webpage at www.amsat.org, by
 calling (888) 322-6728 or by mail to the AMSAT office at 10605
 Concord Street, Kensington, MD 20895, USA.

 Please consider a recurring, club, or corporate donation to maximize
 our chance of success with this mission. Also watch our website at
 www.amsat.org,follow us on Twitter at AMSAT, or on Facebook as
 The Radio Amateur Satellite Corporation for continuing news and
 opportunities for support. AMSAT is a 501(c)3 non-profit corporation
 and donations may be tax-deductible.



 [ANS Thanks AMSAT Board of Directors for the above information]


 -


 /EX

 In addition to regular membership, AMSAT offers membership in the
 President's Club. Members of the President's Club, as sustaining
 donors to AMSAT Project Funds, will be eligible to receive addi-
 tional benefits. Application forms are available from the AMSAT
 Office.

 Primary and secondary school students are eligible for membership
 at one-half the standard yearly rate. Post-secondary school students
 enrolled in at least half time status shall be eligible for the stu-
 dent rate for a maximum of 6 post-secondary years in this status.
 Contact Martha at the AMSAT Office for additional student membership
 information.

 73,
 This week's ANS Editor,
 Joe Spier, K6WAO
 k6wao at amsat dot org

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin -AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Tom Schuessler
I personally am going to ask my local Amateur Radio Club to throw a donation
on the Fox 1C project.  I challenge you to present the same request along to
your own local clubs.

I do numerous Radio Merit Badge presentations for the Boy Scouts and one of
the things I love to do is to throw in a satellite contact opportunity.  Yes
linear passes are fun and very capable, but the concept of showing them that
this kind of technology is available and doable with just a simple hand held
radio and an antenna that you can hold in your hand is much more in the
realm of I could do this too if I had an Amateur Radio license feeling.

Right now, we only one FM bird up there that can be counted on, SO-50, Fox
1A and 1B are still a year off.  (Lituanicasat-1 will be decaying within
days, and maybe two if the French FM satellite opens up soon).  Thus the
opportunities for these basic but, Oh for the Scouts, downright exciting
communication events is quite limited.  The AO-27 contact we did in one of
those Radio Merit Badge workshops (Before it died), sealed the deal for a
Scout and his dad who were attending and they both ended up getting their
tickets.  You can wow them with big ticket equipment and complexity (Smoke
and mirrors), but fun and excitement will get them hooked.  Often times,
simple is better.

An additional challenge for the HEO, MEO and Linear or nothing folks out
there is, instead of buying the next accessory for your already ample
station, give a donation to the FOX project (Or other national AMSAT-esque
project, FM, Linear or Digital), and let's get the ball rolling on many new
opportunities out there just waiting.  You donation may help get another
Scout/young person hooked on our aspect of the hobby.


Tom Schuessler, N5HYP



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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Robert Bruninga
Yes, that is exactly the temperatures of PCSAT in similar eclipse periods.

IE, anything more or less uniformly BLACK (solar panels) no matter the
shape and size will assume that average temperature with 35% eclipses.
This is because the absorbtivity and emissivity of black are both 0.9.
(assuming there is some thermal communication within the spacecraft to move
the heat evenly (such as an aluminum frame)...

If it ever gets into a 0% eclipse period (full sun) those average temps
will rise to about 30-40C.  Still safe for most electronics.

Bob, WB4APR


On Sun, Jul 20, 2014 at 11:09 AM, Graham Shirville 
g.shirvi...@btinternet.com wrote:

 Hi Phil,

 The reality is, even with no battery heater on FUNcube-1 we seem to have
 an acceptable battery temperature of between 0 and +5C. The temp sensor is,
 of course, actually external to the battery itself.

 Our orbit is sun synchronous so we suffer eclipses for approx 33% of the
 orbit ..but then we are relatively close to the earth!

 I would also comment that any active attitude control system will consume
 power...which we don't have much of..

 Probably, if you need continuous operation of the radio system, then a 2U
 with deployable solar panels is the minimum configuration for a CubeSat
 operating on microwave bands with an active attitude control system.

 best 73

 Graham
 G3VZV


 -Original Message- From: g0...@aol.com
 Sent: Sunday, July 20, 2014 3:41 PM
 To: k...@ka9q.net ; amsat-bb@amsat.org ; bruni...@usna.edu
 Subject: Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin -
 AMSAT Fox-1C Launch Opportunity Announced


 I must quickly point out some real data:

 www.warehouse.funcube.org.uk

 Which shows an equilibrium of around +20 degrees after 64 minutes of
 sunlight.
 Black solar cells on a black surface but some polished Aluminium in the
 structure.

 During eclipse, The Earth facing side begins to increase in temperature at
 around -16 degrees, but then cools down rapidly as the cube rotates. The
 temperature is still heading down rapidly as it exits eclipse after 34
 minutes and at around -24C on the outside surfaces.

 Thanks

 David


 -Original Message-
 From: Phil Karn k...@ka9q.net
 To: amsat-bb amsat-bb@amsat.org
 Sent: Sun, 20 Jul 2014 11:59
 Subject: Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin -
 AMSAT Fox-1C Launch Opportunity Announced


 On 07/19/2014 09:23 PM, Robert Bruninga wrote:

  I cannot believe that.  The equilibrium of a nominally black (solar panels
 on all sides) spacecraft is something like about 0 to 30 C (32F to 90F) a
 very benign operational range.  The only time you DO have thermal issues
 is
 when you DO have attitude control and have things that are not equally
 over
 time seeing the sun and dark sky.


 See Dick's paper for the details; I'm just quoting his results. I know
 the basic physics of heat transfer in space but I would never call
 myself an expert. He is.

 But I can do a back-of-the-envelope calculation that tells me he's right.

 The solar cells they're using have an absorptivity and emissivity that
 is both 0.98, as I recall, so a cubesat covered with them is essentially
 a perfect blackbody.

 A blackbody cube with one face normal to the sun at 1 AU will reach an
 equilibrium temperature of -21.35 C. The problem is that the ratio of
 radiating area to absorbing area for a cube is 6:1 (with the sun normal
 to one surface). A sphere would be warmer because its ratio of radiating
 to absorbing area is only 4:1. A thin flat plate normal to the sun (like
 a solar wing) would be even warmer -- 2:1.

 And that -21.35 C figure is for continuous sunlight. Throw in eclipses
 and things get much worse. Yes, it would be a little better when the sun
 shines on a corner rather than normal to a face, and Earth albedo and IR
 radiation will warm things a little, but not enough to matter.

 --Phil

 PS: Temperature of 10 cm blackbody cube at 1 AU:

 Area facing sun: .01 m^2
 Solar constant: 1367.5 W/m^2
 Absorbed power = 13.675 W

 Total radiating area: .06 m^2
 Emissivity = 1.0 (perfect blackbody)
 Stefan-Boltzmann constant = 5.6703e-8 W/(m^2K^4)


 T = (13.675 W / (5.6703e-8 * 1.0 * .06)) ** (1/4)
  = 251.8K == -21.35 C
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Robert Bruninga
Thanks for the FOX-1 thermal data! (36 C variation per orbit)

PCSAT (10 cubesat) has less than 15C variation on its sides  with its 0.6
RPM spin and 35% eclipses, but this is because the sides are made of 1/8
aluminum and have a huge 1/8 center deck that is thermally connected to
the center of each face, providing great communication from the sun side to
the other sides.  Notice, this was a HEAVY satellite because we just
overbuilt it to make sure the heat was evenly distributed.


On Sun, Jul 20, 2014 at 10:41 AM, g0...@aol.com wrote:

 I must quickly point out some real data:

 www.warehouse.funcube.org.uk

 Which shows an equilibrium of around +20 degrees after 64 minutes of
 sunlight.
 Black solar cells on a black surface but some polished Aluminium in the
 structure.

 During eclipse, The Earth facing side begins to increase in temperature at
 around -16 degrees, but then cools down rapidly as the cube rotates. The
 temperature is still heading down rapidly as it exits eclipse after 34
 minutes and at around -24C on the outside surfaces.

 Thanks

 David


 -Original Message-
 From: Phil Karn k...@ka9q.net
 To: amsat-bb amsat-bb@amsat.org
 Sent: Sun, 20 Jul 2014 11:59
 Subject: Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin -
 AMSAT Fox-1C Launch Opportunity Announced

  On 07/19/2014 09:23 PM, Robert Bruninga wrote:

  I cannot believe that.  The equilibrium of a nominally black (solar panels
  on all sides) spacecraft is something like about 0 to 30 C (32F to 90F) a
  very benign operational range.  The only time you DO have thermal issues is
  when you DO have attitude control and have things that are not equally over
  time seeing the sun and dark sky.

 See Dick's paper for the details; I'm just quoting his results. I know
 the basic physics of heat transfer in space but I would never call
 myself an expert. He is.

 But I can do a back-of-the-envelope calculation that tells me he's right.

 The solar cells they're using have an absorptivity and emissivity that
 is both 0.98, as I recall, so a cubesat covered with them is essentially
 a perfect blackbody.

 A blackbody cube with one face normal to the sun at 1 AU will reach an
 equilibrium temperature of -21.35 C. The problem is that the ratio of
 radiating area to absorbing area for a cube is 6:1 (with the sun normal
 to one surface). A sphere would be warmer because its ratio of radiating
 to absorbing area is only 4:1. A thin flat plate normal to the sun (like
 a solar wing) would be even warmer -- 2:1.

 And that -21.35 C figure is for continuous sunlight. Throw in eclipses
 and things get much worse. Yes, it would be a little better when the sun
 shines on a corner rather than normal to a face, and Earth albedo and IR
 radiation will warm things a little, but not enough to matter.

 --Phil

 PS: Temperature of 10 cm blackbody cube at 1 AU:

 Area facing sun: .01 m^2
 Solar constant: 1367.5 W/m^2
 Absorbed power = 13.675 W

 Total radiating area: .06 m^2
 Emissivity = 1.0 (perfect blackbody)
 Stefan-Boltzmann constant = 5.6703e-8 W/(m^2K^4)


 T = (13.675 W / (5.6703e-8 * 1.0 * .06)) ** (1/4)
   = 251.8K == -21.35 C
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Robert Bruninga
Hummh,

We get an equilibrium of a cube to be about 55F (13C) when exposed to the
sun on one side and all the other sides radiating to cold space. (assuming
they are thermally connected).

I wonder why the big difference between our calculations?
Bob, WB4aPR

On Sun, Jul 20, 2014 at 6:59 AM, Phil Karn k...@ka9q.net wrote:

 On 07/19/2014 09:23 PM, Robert Bruninga wrote:

  I cannot believe that.  The equilibrium of a nominally black (solar
 panels
  on all sides) spacecraft is something like about 0 to 30 C (32F to 90F) a
  very benign operational range.  The only time you DO have thermal issues
 is
  when you DO have attitude control and have things that are not equally
 over
  time seeing the sun and dark sky.

 See Dick's paper for the details; I'm just quoting his results. I know
 the basic physics of heat transfer in space but I would never call
 myself an expert. He is.

 But I can do a back-of-the-envelope calculation that tells me he's right.

 The solar cells they're using have an absorptivity and emissivity that
 is both 0.98, as I recall, so a cubesat covered with them is essentially
 a perfect blackbody.

 A blackbody cube with one face normal to the sun at 1 AU will reach an
 equilibrium temperature of -21.35 C. The problem is that the ratio of
 radiating area to absorbing area for a cube is 6:1 (with the sun normal
 to one surface). A sphere would be warmer because its ratio of radiating
 to absorbing area is only 4:1. A thin flat plate normal to the sun (like
 a solar wing) would be even warmer -- 2:1.

 And that -21.35 C figure is for continuous sunlight. Throw in eclipses
 and things get much worse. Yes, it would be a little better when the sun
 shines on a corner rather than normal to a face, and Earth albedo and IR
 radiation will warm things a little, but not enough to matter.

 --Phil

 PS: Temperature of 10 cm blackbody cube at 1 AU:

 Area facing sun: .01 m^2
 Solar constant: 1367.5 W/m^2
 Absorbed power = 13.675 W

 Total radiating area: .06 m^2
 Emissivity = 1.0 (perfect blackbody)
 Stefan-Boltzmann constant = 5.6703e-8 W/(m^2K^4)


 T = (13.675 W / (5.6703e-8 * 1.0 * .06)) ** (1/4)
   = 251.8K == -21.35 C
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Phil Karn
On 07/19/2014 09:23 PM, Robert Bruninga wrote:

 Yes, but with who?  95% of everyone in view is more than 45 degrees OUT of
 the main beam.  Directional antennas have zero value on LEO birds that need
 to serve everyone in view at the same time.  And if you only serve those in
 the main beam, then the duration is under 1 minute.

Run the link budgets. With reasonable numbers (transmit power 100 mW,
range 1,000 km, Rx T = 50K) you only need a few dB of transmit gain to
get megabits/sec into a 60 cm DBS dish at 10 GHz. A few dB can easily
cover an entire hemisphere, though you might want to squash the pattern
to cover it more uniformly (as the GPS satellites do).

The big reason to use attitude control isn't high on-axis antenna gain,
it's AVOIDING ANTENNA NULLS. Fading was the major factor in every one of
the modulation/coding schemes I've designed for AMSAT. It forces me to
use noncoherent (DBPSK) modulation, which even with FEC can cost as much
as 4-5dB over coherent BPSK. And that's WITHOUT fading.

Fading is a major headache in coding design because you need to know how
long a fade will last to know how long to make your interleaver, and you
simply don't know when the spacecraft is unstabilized.

At least I had a good idea with AO-40 because the fading was caused by
the spacecraft spin so it was quite predictable. But ARISSat-1 was
completely unstabilized and I didn't even have an antenna pattern, so I
basically had to pull a maximum fade duration out of my butt.

Same with FOX-1, although it's somewhat less severe in the
data-under-voice mode since it's the fade duration relative to the data
rate that matters, and the data rate in that mode is so extremely low.
But it's a serious problem in the high speed (data only) mode.

And for truly interesting data rates (hundreds of kilobits/sec and up),
slow fading is simply intolerable. Attitude stabilized antennas are the
only way.

--Phil
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Phil Karn
On 07/20/2014 06:27 AM, Rick Walter wrote:
 I was not going to post but since no one else has, I thought there needs to 
 be a correction to a statement made in case some younger people are reading 
 the thread. 
 
 Phil said:
 Good analogy, actually. They returned to the moon six times (succeeding
 on five) because they had excess hardware originally built in the
 expectation that the first attempts would fail.
 
 There were actually seven manned missions to the moon. Six succeeded. Apollo 
 13 never landed on the moon and returned to earth safely. Apollo 
 11,12,14,15,16, and 17 landed. 12 American astronauts walked on the moon. 

That's exactly what I said. They *returned* to the moon (i.e., after
landing the first time on Apollo 11) six times, succeeding on five.

Three missions went to the moon without landing: Apollos 8, 10 and 13,
for a total of nine Apollo lunar missions. Two more (7  9) remained in
earth orbit.

--Phil

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Phil Karn
On 07/20/2014 08:09 AM, Graham Shirville wrote:
 Hi Phil,
 
 The reality is, even with no battery heater on FUNcube-1 we seem to have
 an acceptable battery temperature of between 0 and +5C. The temp sensor
 is, of course, actually external to the battery itself.

You must be using different solar cells, or perhaps you don't fully
cover the exterior with them. I did wonder why Dick didn't consider the
same thing for Fox-1; if you're going to dissipate some of the
electricity they generate in resistance heaters, you might consider
covering less than 100% of the surface with them and cover the remainder
with thermal blankets. I haven't worked out this alternative, and as I
said I'm not a thermal design expert.

At the time I believe Dick said he was considering gold plating the
inside surfaces of the cells to isolate them from the interior, since
there was little or no room for any other kind of insulation. In that
case you would no longer have thermal equilibrium and my back of the
envelope calculation would not apply.

There's one additional factor to make things worse, though I haven't
quantified it. Space-rated solar cells are getting good enough that the
spacecraft as a whole actually converts a non-insignificant amount of
the sunlight hitting it into transmitted RF, and that power is no longer
available to keep the spacecraft warm. So it gets even colder.

That's right, turn on the transmitter and the spacecraft cools down --
at least if the solar cells are not thermally isolated from the interior.

 Our orbit is sun synchronous so we suffer eclipses for approx 33% of
 the orbit ..but then we are relatively close to the earth!

Yes, and you do pick up longwave IR from the earth even on the night
side. According to my copy of Spacecraft Thermal Control Handbook Vol
1, this is only about 150 W/m^2 in LEO, so it doesn't seem to help that
much. Albedo is greater (about 250 W/m^2) but only over the subsolar
point so again it doesn't help much on average.

It *would* help a lot if you could insulate those sides facing dark sky,
and that's where attitude control comes in.

During his after-dinner talk at the AMSAT Symposium a couple of years
ago, astronaut Sam Durrance described just how cold that dark sky is. He
flew with Ron Parise on the Astro-1 and -2 shuttle missions. Because
these were astronomy missions, the shuttle payload bay spent long
periods pointed at dark sky, as opposed to its usual practice (when not
docked to the ISS) of keeping the payload bay toward earth. He said it
got so cold near the orbiter's overhead windows that they had to don
sweaters.

But the real issue that Dick drove home to me in his talk was just how
variable the thermal situation was when you can't control your attitude
and when eclipse durations and beta angles vary so drastically over a
year. Even if you could design for acceptable equilibrium temperatures
under one set of conditions you can't maintain them as they vary so much.

 I would also comment that any active attitude control system will
 consume power...which we don't have much of..

Yes, but active attitude control lets you keep those panels pointed at
the sun to produce much more power on average. Only two of the six
surfaces of a 1U cubesat even need solar cells with my stabilized
design. You can do much better with deployable, steerable panels --
which pretty much demands active attitude control.

The fact that virtually every military, commercial and scientific
spacecraft launched today is three-axis stabilized should settle the
question: active attitude control is the way to go, if you can do it.

--Phil
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-20 Thread Phil Karn
On 07/20/2014 10:00 AM, Paul Stoetzer wrote:

 A good number of
 amateur radio operators are only vaguely aware of the amateur
 satellite program and consider it to be quite esoteric.

Precisely. Huge az/el yagi arrays don't help that image either.

Nor does an occasional, brief, noisy pass of an FM voice-only satellite
carrying 1 QSO at a time do much to impress a young person with a mobile
phone in his pocket that he can use to talk or message anywhere in the
world. The term easysat doesn't seem appropriate when said FM voice
satellite requires pointing an ungainly-looking 2m antenna at the sky
even if that antenna is very small by usual ham satellite standards.
Most mobile phones don't even have visible external antennas anymore.

I'm not trying to make ham radio into a utility to compete with either
the Internet or mobile phones. That's not what it's for. But for those
who'd like to learn, hands-on, about modern communication technology --
for which ham radio *IS* still uniquely suited -- you have to offer
something that's actually halfway modern!

I can't do anything about the occasional, brief passes of a LEO without
going to a higher altitude orbit. But I certainly *can* do far better
with a LEO satellite and a ~1/2 meter ground antenna by:

1. Adding 3-axis attitude control to the spacecraft.
2. Moving up to the microwave bands.
3. Going digital.

Instead of one voice conversation (interrupted by deep, noisy fades) you
could support many. Although the LEO passes would still be occasional
and brief, alternatives to real-time voice would be available. Bulk data
(including recorded and possibly lengthy voice messages) could be sent
up and delivered to an entirely different part of the globe. For those
who don't really care to talk, satellite-generated data (e.g.,
telemetry, imagery) can be multiplexed with the downlink data.

 The bottom line is that AMSAT-NA needs a significant boost in
 membership and visibility and that boost needs to be soon. Putting two
 satellites into orbit that nearly every single ham will be able to
 easily hear (even a $30 Baofeng and it's stock duck should hear high
 passes of the Fox-1 satellites) along with the accompanying publicity
 should provide that boost.

Suppose it were just as easy and cheap to build or buy an amateur
digital microwave satellite earth terminal? In this age of mobile
microprocessors that would at one time have been considered
supercomputers; handheld GPS receivers; Sirius/XM receivers with
postage-stamp antennas; and direct broadcast satellite dishes -- just to
mention a few now-widespread consumer items -- do you really think it so
impossible to set our sights as hams just a little higher than 1960s
technology?

--Phil
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Phil Karn
On 07/18/2014 12:08 PM, Joseph Spier wrote:

 Fox-1C is the third of four Fox-1 series satellites under
 development, with Fox-1A and RadFXsat/Fox-1B launching through the
 NASA ELANA program. Fox-1C will carry an FM repeater system for
 amateur radio for use by radio hams and listeners worldwide. 

YET ANOTHER analog satellite?

I'm not interested.

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Paul Stoetzer
Are FM repeater satellites what we all want in orbit? No. Personally,
I'd like a Mode J linear transponder in a sun synchronous circular
orbit of about 2,000km (if we can't get anything to HEO).

However, the Fox-1A, Fox-1B, Fox-1C, and Fox-1D satellites will
eventually lead to the Fox-2 series of satellites. The software
designed transponders on board the Fox-2 series will be capable of
operating in any number of digital communications modes as well as
operating as linear transponders.

AO-51's V/U FM repeater was probably the most popular amateur
satellite ever launched. Since the loss of AO-51, AMSAT-NA membership
has been declining and is at the point where membership dues alone do
not sustain the operating costs of the organization.

Right now, those who are mildly interested in amateur satellites have
one satellite to try with a minimal investment: SO-50, which is a
satellite that for about half the days of each month is not convenient
for most people who work 9-5 and sleep 10-6 and has a weak downlink
that is often very difficult for newcomers to hear. Even experienced
satellite operators are at times heard to transmit without being able
to hear the satellite. With EO-80 (QB50p2), Fox-1A, and Fox-1C
hopefully in orbit and operational next year, there will be three
easily heard FM satellites (the 9 dB advantage of the 2m downlinks on
these satellites will be quite welcome) - two in sun synchronous
orbits with relatively consistent pass times. Having those satellites
in orbit will mean that more hams get bitten by the satellite bug,
join AMSAT, and progress to improving their stations to operate on the
linear transponders and, potentially, on digital satellites.

Bottom line - an AMSAT with more satellites in orbit means an AMSAT
with more members and that's how we are eventually going to get our
ideal satellites in orbit.

73,

Paul, N8HM

On Sat, Jul 19, 2014 at 2:54 PM, Phil Karn k...@ka9q.net wrote:
 On 07/18/2014 12:08 PM, Joseph Spier wrote:

 Fox-1C is the third of four Fox-1 series satellites under
 development, with Fox-1A and RadFXsat/Fox-1B launching through the
 NASA ELANA program. Fox-1C will carry an FM repeater system for
 amateur radio for use by radio hams and listeners worldwide.

 YET ANOTHER analog satellite?

 I'm not interested.

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Phil Karn
On 07/19/2014 12:28 PM, Paul Stoetzer wrote:
 Are FM repeater satellites what we all want in orbit? No. Personally,
 I'd like a Mode J linear transponder in a sun synchronous circular
 orbit of about 2,000km (if we can't get anything to HEO).

Getting a launch opportunity is difficult and expensive. Going digital
is not.

 However, the Fox-1A, Fox-1B, Fox-1C, and Fox-1D satellites will
 eventually lead to the Fox-2 series of satellites.

I've been hearing that for years, so please forgive my skepticism. Tony
AA2TX himself told me that the analog Fox-1 would be followed by the
digital Fox-2. Now we have Fox-1B, Fox-1C, etc, that will also be
analog. Forgive me if I feel a little like Achilles racing the tortoise.

I originally joined AMSAT as a technical volunteer in mid 1980, shortly
after the Phase III-A launch failure. At the time, AMSAT was doing some
very impressive things. Many weren't even being done (or were just
starting to be done) in the commercial world: the use of digital command
and telemetry links, the use of onboard computers, even the use of
ground computers to steer antennas. AMSAT had shown how to locate an
emergency beacon by measuring its Doppler shift through a LEO
transponder -- which eventually became the SARSAT (Search and Rescue
Satellite) payload on many US and Russian LEO weather satellites.

And AMSAT was showing how to do it all on a low budget, with
resourcefulness replacing brute force bucks. I was blown away by clever
little tricks like spinning a satellite by painting one side of its
antennas black and the other side white. This was ham radio at its best.

But that was 1980. It's now 34 years later and we're still doing the
same old thing. Meanwhile, mobile phones and the Internet have gone from
the exotic to the commonplace -- and I don't have to tell you that
they're 100% digital. TV broadcasting is also now digital, few cable TV
systems still carry analog signals, and FM and shortwave broadcasting
are in a digital transition.

When AMSAT showed how to use an inexpensive hand-held radio to
communicate with a satellite, no one had ever seen such a thing. Now
digital satellite broadcasting and GPS are nearly universal in cars,
hikers and boaters carry SPOT units, and you can buy handheld Iridium
phones that will work anywhere on the globe. All digital, of course.

Yet AMSAT continues to fly one analog satellite after another. Why?

All these outside developments have rendered FCC Part 97.1, the Basis
and Purpose of the Amateur Service, almost completely obsolete with the
singular exception of personal technical education and possibly (some)
emergency communications. You want to further international goodwill by
talking to people in other countries? Get on the Internet. You want to
call your wife to see if she needs anything? Pick up your mobile phone.
Further the technical art? Go work for a communications RD company,
because it isn't happening in ham radio anymore.

How are we justifying our spectrum by doing the same thing over and over
again, while the world passes us by?

Appealing to what the members want doesn't fly with me, because the
members are a tiny fraction of our potential audience. AMSAT keeps
wondering why it can't seem to grow beyond a tiny niche; it need look no
further for the reason.

Nor does an appeal to simplicity and cost carry any weight. Mobile
phones, GPS units and Sirius/XM receivers may not be simple but that
doesn't keep them from being cheap and easy to use. It's their very
complexity (if you consider digital to be complex -- which I don't)
that makes them cheap and easy to use.

But by design they are impossible to take apart and learn from. That's
where the amateur service can still play a big role. For those who want
to learn communications technology by hands-on experimentation there is
still simply nothing like it. But where are the amateur digital voice
satellite systems to take apart and study? At least a linear transponder
could repeat an efficient digital signal, but with the trend to FM even
that is no longer possible. If an amateur satellite carries any digital
links at all, they are slow and generally limited to telemetry and
command, not user-to-user communications. Many don't even use modern
modulation and error-correction methods, making them that much harder to
access with the small antennas to which most hams are now limited
because of CCRs and other restrictions.

Far from being elitist or hard to use, digital represents the *only*
way forward. It's time to move into the 21st century.

--Phil

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Andrew Glasbrenner

Getting a launch opportunity is difficult and expensive. Going digital is
not.

The Fox satellites each have four designated experiment cards. Assemble a
team and pitch a proposal for 1D, or 1C if you can do it in a hurry. 

73, Drew KO4MA

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread John Becker


On 7/19/2014 1:54 PM, it was wrote:

YET ANOTHER analog satellite? I'm not interested.

I hear yeah !




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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Jerry Buxton

On 7/19/2014 3:24 PM, Phil Karn wrote:

However, the Fox-1A, Fox-1B, Fox-1C, and Fox-1D satellites will
eventually lead to the Fox-2 series of satellites.

I've been hearing that for years, so please forgive my skepticism. Tony
AA2TX himself told me that the analog Fox-1 would be followed by the
digital Fox-2. Now we have Fox-1B, Fox-1C, etc, that will also be
analog. Forgive me if I feel a little like Achilles racing the tortoise.
Ah, but the plan always was to build four of the Fox-1 series, which is 
a series of FM analog transponders.  Initially, one had a launch and the 
other three would be ready to fly if other opportunities came up.  If 
you're going to spend the time developing them, why not partner for free 
launches (ELaNa) for more than one?  The opportunities for an FM 
transponder and educational outreach are good.  I still have 
universities looking to partner.


Look at it this way... we are clearing the shelves with 3 out of 4 of 
the intended Fox-1 going to orbit, that really means that we can pretty 
much call it a day with Fox-1 and move on to Fox-2 now.  We will build 
them all and be done with them all by next May.  There will be more than 
one flying soon, so that we can learn how well they work and apply those 
lessons to Fox-2 while we're working out the design.  It's only the 
beginning!


Jerry Buxton, NØJY

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread JoAnne Maenpaa
Hey, this sounds like a terrific opportunity. Not only did AMSAT work
on securing our new launch opportunities ... but we are in a position
to offer a launch opportunity for a mode/radio/experiment for those
who can contribute to amateur radio in space instead of complain about
it.

--
73 de JoAnne K9JKM
k9...@amsat.org 

-Original Message-
From: amsat-bb-boun...@amsat.org [mailto:amsat-bb-boun...@amsat.org]
On Behalf Of Andrew Glasbrenner
Sent: Saturday, July 19, 2014 15:43
To: 'Phil Karn'; 'Paul Stoetzer'
Cc: amsat-bb@amsat.org
Subject: Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin -
AMSAT Fox-1C Launch Opportunity Announced


Getting a launch opportunity is difficult and expensive. Going
digital is
not.

The Fox satellites each have four designated experiment cards.
Assemble a
team and pitch a proposal for 1D, or 1C if you can do it in a hurry. 

73, Drew KO4MA

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Phil Karn
On 07/19/2014 01:42 PM, Andrew Glasbrenner wrote:
 
 Getting a launch opportunity is difficult and expensive. Going digital is
 not.
 
 The Fox satellites each have four designated experiment cards. Assemble a
 team and pitch a proposal for 1D, or 1C if you can do it in a hurry. 
 
 73, Drew KO4MA
 

I see no reason to consider a digital satellite an experiment. Not in
2014, anyway.

Besides, there are several other critical technical hurdles AMSAT must
first overcome if we are to do anything interesting with a cubesat.
First and foremost among them is

ATTITUDE CONTROL!

Passive bar magnets (or nothing at all, as on ARISSat-1) no longer cut it.

The lack of attitude control forces us to use simple omnidirectional
antennas, which in turn keeps us on the crowded and narrow VHF/UHF
bands. Worse, there's really no such thing as an omnidirectional
antenna so our links are plagued by frequent deep fades of unlimited
(or at least unknown) duration. Fading has driven every one of my
modulation/coding designs for AMSAT telemetry links -- at the expense of
making them much less power-efficient.

And power efficient means smaller ground antennas, and that means a
cheaper and more accessible ground station for the average ham. And THAT
means a much larger potential AMSAT membership.

With attitude control, our satellite could use directional antennas on
the microwave bands. Directional antennas on higher frequencies mean
much better link budgets. You could easily do MEGABITS PER SECOND
between LEO and small ground antennas!

A lack of attitude control also plagues thermal design. I learned this
from Dick Janssen KD1K's talk at the Symposium a few years ago when he
said Fox-1 was the most difficult thermal design he'd ever done for
AMSAT. And he's done many.

The problem is that without attitude control you have to cover every
available surface with solar cells to guarantee power in any attitude,
and solar cells are excellent thermal radiators. Those not facing the
earth or the sun face dark sky, radiating away much of the spacecraft's
heat. I think he found the equilibrium temperature of a 1U cubesat to be
something like -30 or -40 C! The team had no choice but to add
resistance heaters to keep the payload (especially the batteries) warm.
I can't think of a more painful use of scarce, hard-earned, expensive DC
power in space.

Attitude control would completely solve this problem too. In LEO the
most common form of attitude control is local vertical/local
horizontal, the mode the ISS uses most of the time. You'd designate one
face as nadir-pointing; here you would mount antennas and earth
observation cameras. With circularly polarized antennas, you'd still
have a degree of freedom around the yaw axis, i.e., you could rotate
around the local vertical with no effect on the RF links.

The opposite (zenith-facing) side would have a solar cell, as would one
of the four remaining sides. The remaining three would be covered with
thermal blankets to insulate the spacecraft from the dark sky they'd
face all the time. (Not being a thermal designer I haven't calculated
what the new equilibrium temperature would be. But it would obviously
solve Dick's problem. He might even have to leave part of those surfaces
exposed to radiate excess heat!)

You see how this works? At low beta angles, when the sun is in or near
the orbital plane, you point the side with the solar cell forward at
local sunrise. At local noon you yaw 180 degrees so the cell faces the
sun as it sets behind you. At higher beta angles you simply yaw to track
the sun as it passes off to one side; in the limiting case of a beta
angle of 90 degrees (continuous sunlight) you'd simply keep the
spacecraft yawed at a constant +90 or -90 degrees.

And you only need to buy two expensive solar cells instead of (nearly) six.

Attitude control systems for cubesats already exist. You can buy one for
$200,000 from suppliers serving the burgeoning cubesat community (most
of which considers ham radio completely irrelevant except as a source of
free spectrum). But that's not the AMSAT way. I am sure that if we
brought enough clever minds together (along with some good mechanical
engineers and craftsmen) we could design and build our own attitude
control system for far less.

But to attract all those people to do all these new (in AMSAT) things,
you have to stop doing the same old thing over and over. You have to
make a conscious choice to stand back and actually innovate at the
systems level instead of relegating digital to the status of an
experiment on the same old primitive spacecraft bus.

Look at all the attention and excitement generated by the ISEE-3 Reboot
project. That's because they're actually doing something new and
challenging. They say they've gotten donations from many people far
outside the usual space groupie segment of the population. It's also
caught the imagination of at least a few hams, including the AMSAT-DL
gang which has been using their 20m Bochum dish to 

Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Phil Karn
On 07/19/2014 02:04 PM, Jerry Buxton wrote:

 other three would be ready to fly if other opportunities came up.  If
 you're going to spend the time developing them, why not partner for free
 launches (ELaNa) for more than one?  The opportunities for an FM
 transponder and educational outreach are good.  I still have
 universities looking to partner.

Ah, because launches are scarce and expensive, and (re)developing even
the same old thing consumes much of AMSAT's limited resources. And
they're limited because we have yet to interest more than a tiny niche
in what we're doing.

It's great to have universities looking to partner, but what do they
bring to the table, really? Are we sure they're not just looking for
free spectrum?

 one flying soon, so that we can learn how well they work and apply those
 lessons to Fox-2 while we're working out the design.

We already know how well they'll work because we've done the same thing
many times before. I hate to say it, but this is no longer rocket
science. The physics is well understood, and those same physics tell us
how we could accomplish so much more with our (currently) limited resources.

--Phil

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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Jerry Buxton

On 7/19/2014 4:50 PM, Phil Karn wrote:

Ah, because launches are scarce and expensive, and (re)developing even
the same old thing consumes much of AMSAT's limited resources. And
they're limited because we have yet to interest more than a tiny niche
in what we're doing.


But you arguing about something that has already happened.  That makes 
no sense.
Arguing for doing something different, as you also did just a bit ago 
today, makes sense.
Why did the U.S. go back to the moon so many times?  I don't know. But 
we did, and that is done.  You could argue now that it had been done 
before, why did we do it over and over, it was the same old thing.  That 
doesn't change the facts.

There is an audience for these FM satellites.

It's great to have universities looking to partner, but what do they
bring to the table, really? Are we sure they're not just looking for
free spectrum?
Both universities that I am working with are building amateur radio 
ground stations and interesting the students in becoming hams.  We all 
benefit from that.  And some other universities want to fly an ADAC 
system.  We may benefit from that on Fox-2.

one flying soon, so that we can learn how well they work and apply those
lessons to Fox-2 while we're working out the design.

We already know how well they'll work because we've done the same thing
many times before. I hate to say it, but this is no longer rocket
science. The physics is well understood, and those same physics tell us
how we could accomplish so much more with our (currently) limited resources.
We have already learned a great deal from an engineering process 
perspective, as well as about cramming a lot into a little cubesat. Not 
rocket science, but certainly for a large all volunteer group a valuable 
step toward what it will take to build something more complex.  I think 
you over estimate the ability of an all-volunteer workforce, in terms of 
churning out satellites akin to how a business does it.  Amateur radio 
is a hobby!


You see lemons.  I see lemonade.  But by all means, let's go for pink 
lemonade and keep on talking about Fox-2 opportunities while people 
enjoy what we have already done with the Fox-1 series!


Jerry Buxton, NØJY



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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Phil Karn
On 07/19/2014 03:32 PM, Jerry Buxton wrote:

 But you arguing about something that has already happened.  That makes
 no sense.

None of the Fox satellites have yet flown, so they haven't already
happened.

 Why did the U.S. go back to the moon so many times?  I don't know. But
 we did, and that is done.  You could argue now that it had been done
 before, why did we do it over and over, it was the same old thing.  That
 doesn't change the facts.

Good analogy, actually. They returned to the moon six times (succeeding
on five) because they had excess hardware originally built in the
expectation that the first attempts would fail.

And when they did return, they began to do some serious scientific
exploration that made it worthwhile. Unfortunately, the public *did* see
this as the same old thing and Congress quickly withdrew support. As
everyone knows, NASA canceled the last three Apollo lunar missions and
humans haven't left earth orbit since Apollo 17. (Strictly speaking,
even Apollo never left earth orbit, since the moon orbits the earth.)

Yet NASA has always managed to find support for new and interesting
things in space even without a human presence. The two keys to public
interest have always been 1) exploration and 2) photography.

Apollo certainly did that in its time. More recently, stunning pictures
from the surface of Mars and of the moons and backlit rings of Saturn
have done much to keep NASA going even as it flails aimlessly in its
human program. Sure, the ISS returns some pretty good pictures of earth
but so do many robotic spacecraft. And the ISS certainly isn't exploring
much of space from only 400 km up. That's why most people don't find it
very exciting.

 Both universities that I am working with are building amateur radio
 ground stations and interesting the students in becoming hams.  We all
 benefit from that.  And some other universities want to fly an ADAC
 system.  We may benefit from that on Fox-2.

I'm hearing privately that many university groups really are after us
for only our spectrum. Or our spectrum plus a ready-made
telecommunications system they can use for their purposes without having
to worry about the details. I actually don't oppose this categorically
as some do, but I insist on *some* benefit back to the amateur service,
such as an interesting new communications system to experiment with and
to learn from. Some aren't even willing to go that far.

--Phil
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Re: [amsat-bb] ANS-199 AMSAT News Service Special Bulletin - AMSAT Fox-1C Launch Opportunity Announced

2014-07-19 Thread Robert Bruninga
 The lack of attitude control forces us to use simple omnidirectional

 antennas, which in turn keeps us on the crowded and narrow VHF/UHF
 bands. Worse, there's really no such thing as an omnidirectional
 antenna so our links are plagued by frequent deep fades of unlimited
 (or at least unknown) duration. Fading has driven every one of my
 modulation/coding designs for AMSAT telemetry links -- at the expense of
 making them much less power-efficient.

 And power efficient means smaller ground antennas, and that means a
 cheaper and more accessible ground station for the average ham. And THAT
 means a much larger potential AMSAT membership.


 With attitude control, our satellite could use directional antennas on
 the microwave bands. Directional antennas on higher frequencies mean
 much better link budgets.

Yes, but with who?  95% of everyone in view is more than 45 degrees OUT of
the main beam.  Directional antennas have zero value on LEO birds that need
to serve everyone in view at the same time.  And if you only serve those in
the main beam, then the duration is under 1 minute.

 A lack of attitude control also plagues thermal design
 I think he found the equilibrium temperature of a 1U cubesat
 to be something like -30 or -40 C!

I cannot believe that.  The equilibrium of a nominally black (solar panels
on all sides) spacecraft is something like about 0 to 30 C (32F to 90F) a
very benign operational range.  The only time you DO have thermal issues is
when you DO have attitude control and have things that are not equally over
time seeing the sun and dark sky.

PCSAT is now 13 years in orbit and the above range is what it sees.  And
that range is over a 2 month period.  THe orbit-by-orbit temperature
changes are less than +/- 10 degrees C.  The extremes are due to the
seasons of the orbit.  When it is seeing eclipses it averages to about
10C and when it is in full sun for weeks at a time, it gets up to 30 C (90F)

I do agree that attitude control is nice to have, but my point is that it
only makes the thermal problem much worse and that gain is of no value
for a LEO where it must see everyone in a footprint at the same time.
(Remmebr you cannot have wide beamwidth and gain at the same time).

Gain for HEO's of course is another matter! (think AO-10, AO-13 and AO-40)

Bob, WB4APR
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