[amsat-bb] PSLV C-18 Launch successful

2011-10-11 Thread Mani VU2WMY

Hello All,
The PSLV C-18 Mission is a Grand success. All the four satellites were  
successfully injected into their precise orbits.
The Jugna was injected at 05:56 UT and the beacon will turn ON at  
06:31 UT. It is expected that the Jugnu at that time should be  
somewhere over N.W of South America. Any early signal report 0n  
437.275 CW from around this part of the World would be greatly  
appreciated.


73 de

Mani, VU2WMY
Secretary & Station-In-Charge
Upagrah Amateur Radio Club VU2URC
ISRO Satellite Centre
HAL Airport Road, Bangalore-560 017.
Phone:(O)91-80-25082054/2598/2192
Mobile:  91-80-98803 41456
E-mail ID: w...@isac.gov.in
   vu2wmy_m...@yahoo.com
   isroh...@yahoo.com

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[amsat-bb] SRMSAT

2011-10-11 Thread Sanjay Srikanth Nekkanti
Dear Folks,

"SRMSAT" a Nano Satellite from SRM University and "Jugnu" from IIT kanpur,
India have been successfully placed in orbit at 11:32 Am IST. I would
request the Hams all over the world to track the satellites and send in the
beacon data to the following address.

kc2...@arrl.net   and
sanjaynekka...@gmail.com

SRMSAT beacon is at  437.425 MHz
Jugnu beacon is at 437.275 MHz
 Thanking you,





73
AB3OE,
Sanjay Srikanth Nekkanti.
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[amsat-bb] Re: ARISsat-1

2011-10-11 Thread Alan Cresswell

ARISsat performance.

Very poor performance of ARIssat over ZL today (7 passes.).  All passes in
Low Power Mode except the last which was in Emergency mode.  All passes were
fully sunlit and had been on for 30 minutes or more before my AOS.  A few
went to high power mode for a minute or two mid pass but quickly reverted to
low power mode.

Alan
ZL2BX

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[amsat-bb] Re: KickSat - a personal spacecraft of your own in space

2011-10-11 Thread Zac Manchester
Hi All,

In response to Trevor's questions, the current board design is about
3.2 cm x 3.2 cm x 4 mm.  At that size, we can fit about 200 in a 1U
CubeSat (stacked 3x3x22).  We're pretty sure we can thin that down a
little more by using thinner PCBs.  If we get way more than 200, we
can always go to a 2U or 3U CubeSat.

What I'd really like to do, however, if we can get enough sponsors, is
to make a custom ASIC.  If we can make custom silicon, we can get the
size and the price way down.  This may not be realistic this time
around, but it is something I really want to pursue if I can get the
money.

As far as power, the Sprites are around 10 mW, and yes, they need
solar power, so they won't operate through eclipse.  They do, however
have a bank of capacitors to buffer the power coming out of the solar
cells, so tumbling won't be a problem.

Thanks,
Zac
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[amsat-bb] Satellite Beacon Tracking Request

2011-10-11 Thread Mani VU2WMY

Dear friends,

As you all might be aware that two cubesats 'Jugnu' and 'SRMSat' using  
amateur frequencies are to be launched by PSLV C-18 from Satish Dhawan  
Space Centre [SDSC], Shriharikota, India. The expected launch time is  
05:30 UT.

In this regard, I'm herewith forwarding the mail from Mr. Shantanu  
Agarwal, Team Lead for the 'Jugnu', requesting the Global Amateur  
Radio fraternity to provide the CW Beacon signal Report along with the  
plain decoded morse message, if possible.

Any help in this regard would be greatly appreciated, as this would be  
very helpful to evaluate various ob-board system performance.

'Jugnu' beacon is at 437.275 MHz, OOK.

The reports can be sent to the following mail ID.s
w...@isac.gov.in[1]
shan...@iitk.ac.in[2]

The predicted TLE's:

JNU
1 9U 11072A   11285.2472  .1785  0-0  96625-3 0  1235
2 9  20.0506  66.7109 0018405   5.1080 190.7439 14.1133892219
SRM
1 8U 11072A   11278.34967500  .1077  0-0  60876-3 0  1233
2 8  20.0603  97.4017 0010015 338.6461 208.4324 14.0919996814

Thanks in advance and looking forward to your valuable reports.

73 de

Mani, VU2WMY
Secretary & Station-In-Charge
Upagrah Amateur Radio Club VU2URC
ISRO Satellite Centre
HAL Airport Road, Bangalore-560 017.
Phone:(O)91-80-25082054/2598/2192
Mobile:  91-80-98803 41456
E-mail ID: w...@isac.gov.in[3]
vu2wmy_m...@yahoo.com[4]
isroh...@yahoo.com[5]

- Forwarded message from shan...@iitk.ac.in[6] -
Date: Tue, 11 Oct 2011 20:06:56 +0530
From: Shantanu 
 Subject: Satellite Beacon Tracking Request
  To: w...@isac.gov.in[8]

Dear Sir,

We will be thankful if you can track our satellite beacon after launch.

You are requested to kindly post our satellite details on various HAM
groups to track our satellite beacon after launch.

Our satellite beacon is at 437.275 MHz, OOK.

Thanks.
Shantanu Agarwal

- End forwarded message -



Links:
--
[1] mailto:wmy%40isac.gov.in
[2] mailto:shantag%40iitk.ac.in
[3] mailto:wmy%40isac.gov.in
[4] mailto:vu2wmy_mani%40yahoo.com
[5] mailto:isrohams%40yahoo.com
[6] mailto:shantag%40iitk.ac.in
[7] mailto:shantag%40iitk.ac.in
[8] mailto:wmy%40isac.gov.in


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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Bob Bruninga
> Question, what is the closest spacing for geo 
> satellites to share the same slot?  
> Is this theoretically practical and or possible?

I think someone already said that there are no such thing as physical slots.  
Slots are FREQUENCY based.  Meaning their separation only has to be as great as 
the beamwidth of the grouind based antennas that will use them IF they are on 
he SAME frequency.

So "C" band satellites were originally at 4 degree separation (10 foot dishes) 
then went to 2 degree separation by making evrey other TV channel be oppositely 
polarized.

Such spacing only applies to large constellatiosn of birds on the SAME 
identical frequency plans.  (such as consumer TV downlinks).

If we had ground receive antennas that had beamwidths the width of the moon, 
then we couild have nearly 720 slots (each 0.5 deg wide).  If a GEO 
constellation used laser communications links, with user ground stations using 
OPTICAL telescopes, there could be a million slots because the telescopes could 
resolve them down to .0003 degrees?

Oh, for HAMS with an OSCAR array and beamwidths of say 30 degrees, then there 
could be 12 slots.

Bob, WB4APR
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[amsat-bb] Endeavour's Pink Slip Transferred

2011-10-11 Thread Clint Bradford
Michael Curie 
Headquarters, Washington 
202-358-1100 
michael.cu...@nasa.gov 
RELEASE: 11-343

NASA TRANSFERS ENDEAVOUR TITLE TO CALIFORNIA SCIENCE CENTER

WASHINGTON -- NASA transferred title and ownership of space shuttle 
Endeavour to the California Science Center (CSC) during a ceremony 
Tuesday at the center in Los Angeles. The transfer is the first step 
toward CSC receiving Endeavour in the latter half of 2012. 

"NASA is pleased to share this wonderful orbiter with the California 
Science Center to help inspire a new generation of explorers," NASA 
Administrator Charles Bolden said. "The next chapter in space 
exploration begins now, and we're standing on the shoulders of the 
men and women of the shuttle program to reach farther into the solar 
system." 

Bolden announced April 12 that CSC was one of four institutions 
nationwide to receive a shuttle. After display preparation and 
post-mission work are complete, NASA will deliver Endeavour on the 
747 shuttle carrier aircraft to Los Angeles International Airport. 
>From there, the shuttle will be driven through the streets of Los 
Angeles to its destination at the Science Center in Exposition Park. 

"Endeavour now will begin its new mission to stimulate an interest in 
science and engineering in future generations at the science center," 
California Science Center President Jeffrey Rudolph said. 

For information about where all the retired space shuttles will be 
displayed, visit: 



http://www.nasa.gov/mission_pages/transition/placement/index.html 


-end-


Clint Bradford
clintbradf...@mac.com




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[amsat-bb] KiwiSAT Camera

2011-10-11 Thread Fred Kennedy
Hi Guys,
Been asked by the student that is running some tests on the very simple 
camera that we are 
installing on KiwiSAT, what the cost would be of a commercial satellite 
surveillance camera. 
   He has not found any prices despite web searching - and I haven't done much 
better!  
  He wants to contrast the cost of our simple unit to a proper industrial one 
in a .ppt  presentation on 
his findings.
  Can someone out there in the business give us an idea of the range from the 
simplest to the most 
sophisticated? (Has to be mega bucks!)
( Cost of ours ?- about $100!  But flown successfully and  reliably (for 
our purpose) on several 
Cubesats!!!)
  Thanks
 Fred Kennedy
 ZL1BYP
 KiwiSAT Project Leader   
   

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[amsat-bb] India PSLV C-18 Launch with Jugnu and SRMSAT Webcast

2011-10-11 Thread JoAnne Maenpaa
Hello Everyone,

Here is one news item that will happen before the weekend ANS bulletins are
sent out:

The PSLV C-18 launch from India's Satish Dhawan Space Centre [SDSC], in
Shriharikota, India will be webcast live at http://www.isro.org/. The
expected launch time is 05:30 UTC October 12. 

The Jugnu team is requesting CW beacon signal reports along with the plain
decoded morse message be sent to the following mail IDs:
w...@isac.gov.in
shan...@iitk.ac.in

The SRMSat reports can be sent to:
sanjaynekka...@gmail.com

Jugnu Frequency:  CW Beacon - 437.275 MHz (17dbm)
SRMSAT Frequency: CW Beacon - 437.425 MHz (10dbm)

Preliminary TLEs from ISTRAC (ISRO Telemetry, Tracking and Command Network):

SRM 
1 9U 11072A 11278.34967500 .1077 0-0 60876-3 0 1233 
2 9 20.0603 97.4017 0010015 338.6461 208.4324 14.09199968 14
http://www.amsat.org/amsat/archive/amsat-bb/48hour/msg90110.html (amsat-bb)

More information and a countdown clock can be found on-line at:
http://srmsat.in/

--
73 de JoAnne K9JKM
k9...@amsat.org 
Editor, AMSAT News Service



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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Ken Ernandes
What you're describing is the AMSAT Phase 3 paradigm which IMHO is still the 
most viable way to go.  

I would never say never, but we (AMSAT) haven't had great success with 
propulsion systems in our amateur satellites.  That is why I'd like to have 
more experience with successful propulsion events in Molniya-like orbits before 
I'd recommend attempting maintaining a GEO orbit.

73, Ken N2WWD

Sent from my iPad



On Oct 11, 2011, at 4:41 PM, Joe  wrote:

> How hard (Energy) budget is it to have that giant elliptical orbit,  I can't 
> remember what bird had it,  but it was an orbit named like moylina or 
> something like that  where the perigee was very low but the apogee was like 
> WAY out there giving passes that were extremely long.
> 
> Joe WB9SBD
> 
> The Original Rolling Ball Clock
> Idle Tyme
> Idle-Tyme.com
> http://www.idle-tyme.com
> 
> On 10/11/2011 3:27 PM, Gordon JC Pearce wrote:
>> On Tue, 11 Oct 2011 15:08:01 -0400
>> Ken Ernandes  wrote:
>> 
>> 
>> 
>>> I hope this is somehow helpful in understanding what AMSAT would really be 
>>> up against if it  wanted to have an independent GEO satellite or consider a 
>>> sub-GEO drifting orbit.
>> Thank you Ken, for the rocket scientist's take on it ;-)
>> 
>> It's refreshing to hear someone who actually has sat down and done the maths 
>> comment on how easy or hard it would be to put a satellite into a high orbit.
>> 
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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Trevor .
--- On Tue, 11/10/11, Joe  wrote:
> How hard (Energy) budget is it to have that giant elliptical orbit,  
> I can't remember what bird had it,  but it was an orbit named like 
> moylina or something like that  where the perigee was very low
> but the apogee was like WAY out there giving passes that were 
> extremely long.

It's a great orbit, AO-40 was aiming for it. 

Bottom line is cost - $10-15 million for launch to Geo transfer orbit and then 
costs of incorporating and controlling a motor on the sat to get it to Moylina. 

You should be able to build the sat for a million or so - it's the launch costs 
that are the killer.

73 Trevor M5AKA


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[amsat-bb] Re: SatPc32 kepler Data

2011-10-11 Thread George Henry
I'm guessing you're running XP on that computer?  If so, the kepler folder is 
now (v12.8) located at C:\Documents and Settings\Owner\Application 
Data\SatPC32\Kepler where "Owner" is the profile name you sign on with.


George, KA3HSW




- Original Message 
> From: Howard Kowall 
> To: amsat-bb@amsat.org
> Sent: Tue, October 11, 2011 2:49:10 PM
> Subject: [amsat-bb] SatPc32 kepler Data
> 
> Hello all
> I have an older laptop that has no internet connection,I run  Satpc32 on my 
>main computer that has internet connection and I am able to update  the kepler 
>data.I want to use the  kepler data from my main computer,and  copy it to my 
>laptop via USB  flash drive.I cant seem to find the kepler  folder in the 
>SatPc32 folder.Has anyone one shared the kepler data.
> Thanks to  all who read and reply in  advance
> Howard
> VE4ISP
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[amsat-bb] Re: SatPc32 kepler Data

2011-10-11 Thread Mark L. Hammond
Howard,

This depends on your OS and the version of SatPC32.  On more current versions 
of both software and OS, the folders are HIDDEN by default, so you to make sure 
you have can see all files (it's Windows Folders option).   It's a tad 
annoying...so get those files unhidden. 

On a Windows7 system using SatPC32 12.8a, the files are here (where username is 
the name of the user account in Win7).

C:\Users\username\AppData\Roaming\SatPC32\Kepler

(In the SatPC32 window where you select the keps files---you can see the path 
at the bottom of the window...)

Hope that helps :)

73,

Mark N8MH 


At 02:49 PM 10/11/2011 -0500, Howard Kowall wrote:
>Hello all
>I have an older laptop that has no internet connection,I run Satpc32 on my 
>main computer that has internet connection and I am able to update the kepler 
>data.I want to use the  kepler data from my main computer,and copy it to my 
>laptop via USB  flash drive.I cant seem to find the kepler folder in the 
>SatPc32 folder.Has anyone one shared the kepler data.
>Thanks to all who read and reply in advance
>Howard
>VE4ISP
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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Joe
How hard (Energy) budget is it to have that giant elliptical orbit,  I 
can't remember what bird had it,  but it was an orbit named like moylina 
or something like that  where the perigee was very low but the apogee 
was like WAY out there giving passes that were extremely long.


Joe WB9SBD

The Original Rolling Ball Clock
Idle Tyme
Idle-Tyme.com
http://www.idle-tyme.com

On 10/11/2011 3:27 PM, Gordon JC Pearce wrote:

On Tue, 11 Oct 2011 15:08:01 -0400
Ken Ernandes  wrote:




I hope this is somehow helpful in understanding what AMSAT would really be up 
against if it  wanted to have an independent GEO satellite or consider a 
sub-GEO drifting orbit.

Thank you Ken, for the rocket scientist's take on it ;-)

It's refreshing to hear someone who actually has sat down and done the maths 
comment on how easy or hard it would be to put a satellite into a high orbit.


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[amsat-bb] Re: SatPc32 kepler Data

2011-10-11 Thread Dee
Howard,
I was curious since I seem to remember these as you do.
I looked at the download screen and it points to:
C:\users\name of user\appdata\roaming\satpc32\kepler\
My user name happens to be "DEE"
Hope you find it.
73,
Dee, NB2F

-Original Message-
From: amsat-bb-boun...@amsat.org
[mailto:amsat-bb-boun...@amsat.org] On Behalf Of Howard Kowall
Sent: Tuesday, October 11, 2011 3:49 PM
To: amsat-bb@amsat.org
Subject: [amsat-bb] SatPc32 kepler Data

Hello all
I have an older laptop that has no internet connection,I run
Satpc32 on my main computer that has internet connection and I
am able to update the kepler data.I want to use the  kepler
data from my main computer,and copy it to my laptop via USB
flash drive.I cant seem to find the kepler folder in the
SatPc32 folder.Has anyone one shared the kepler data.
Thanks to all who read and reply in advance Howard VE4ISP
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[amsat-bb] Re: Geostationary Satellites-HEO MEO

2011-10-11 Thread Dee
All,
As most of you know me, I am one of the voices in the crowd
within  satellite circles and have been accused of having my
own agenda.  I am a fixture at many hamfests here in the New
Jersey Area and wherever I can present to the Amateur
community the aspects of satellite activity and promote
AMSAT's proliferation.  I give many talks and dog and pony
shows to various clubs.  My motto is "I work for donations!"
I am glad this thread was ongoing since I come across this
type of thinking all the time.  It's a good discussion since
AMSAT membership is declining and Satellite enthusiasm is
dwindling, so I read.

While this area of insuring plans for HEO and MEO birds is one
of my pet projects, AMSAT itself has re-addressed itself to
LEO activities because of financial reaches that present
launches are out of the normal  (?) abilities of AMSAT to
obtain.  My many unscientific polls as to why hams are not
rejoining AMSAT nor assisting future funding shows that they
think we have to put up HEO or MEO birds to attract them back
into the fold.  Of course this doesn't make sense and it
doesn't add to our present coffers to even think about these
type of birds.  Yes, it costs money to do these things.

In the past, there were negotiations behind the scenes with a
GEO-Sync satellite company to add our payload to one of these
birds.  Company was sold, contacts were lost and so went that
avenue.  As with an AO-40 type satellite, we had numerous
items made by our supporting volunteers and many, many, many
volunteer hours to see that satellite came to fruition.
Volunteers even gave up precious vacation time to work on this
project.   A minimal cost launch by Arianne certainly provided
a great opportunity.  Some of our people went by the wayside
since then and we lost engineering staff to fall back on.

As Dan, N8FGV, points out to us all is that our dreams are
still there.  We need to reactivate those spirits  as he
indicates.  One person stated, "I am willing to ante up
$4000-I need to convince 4,999 of my friends to do the same."
We are all Amateurs in this satellite area and as pioneers in
Ham Radio, we must reinvent ourselves to continue to be
prominent in building sats with real actual launches rooted
out where we can.  We have dedicated people now in active
building projects for slots available for launch.  My hat is
off to them and I will always support their efforts.  Having
functioning packages on the ready is a big plus-  Look at
ARISsat-1 and that was a super job by "OUR" staff to step up
and act before the deadline.  (We don't need no stinkin' UHF
antenna!) (OOPS?)

Dan provides us with answers to all these questions of why and
why not.  Read his input as well and I think this thread needs
the answer of how much is the Amateur community willing to
contribute to keep these higher orbiting satellite ideas
alive.  Anyone have a "RICH" uncle to donate something to this
superfund?  I think that we need a spark - incentive - or a
benefactor to step up to get us on the launch pad at the right
spot.  Lottery tickets seem to be the American dream (HI, HI).
Please feel free to "thank" our many sincere volunteers that
keep publications coming, transponders appearing, protecting
frequency allocations, monitoring rule proposals, Symposiums
happening and informational updates accurate.
73,
Dee, NB2F
NJ AMSAT Coordinator

-Original Message-
From: amsat-bb-boun...@amsat.org
[mailto:amsat-bb-boun...@amsat.org] On Behalf Of Daniel
Schultz
Sent: Tuesday, October 11, 2011 2:03 AM
To: amsat-bb@amsat.org
Subject: [amsat-bb] Re: Geostationary Satellites

It is true that a Geo bird would only cover 1/3 of the Earth,
but it would ALWAYS be there, with no need for antenna rotors
or keps or a computer for tracking. It would be like picking
up a telephone. It would be wonderful for emergency service in
a disaster area. It could provide high speed digital
communications on the amateur microwave bands in places where
the internet is not available.

Geosynchronous orbit slots are allocated by transponder
frequency. On the amateur radio bands we are free to locate a
satellite anywhere we can get to because we don't share our
frequencies with commercial transponders.

The reason we don't have any high altitude satellites is all
about the money.
We amateurs created the small satellite business. Back in the
old days the big boys laughed at our cute little toy
satellites, but they did allow us to bolt them to a launch
vehicle for free or for very low cost. The experts were
certain that our homebrew satellites wouldn't last a week
without expensive mil-spec electronic components. We amateurs
proved that small satellites were useful and thus created a
market that we are now priced out of. The launches that used
to be free can now be sold to paying customers for millions of
dollars. Many of the companies in the small satellite business
were founded by Amsat alumni.

We amateurs are a non-commercial service, by law, with no
product or serv

[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Gordon JC Pearce
On Tue, 11 Oct 2011 15:08:01 -0400
Ken Ernandes  wrote:



> I hope this is somehow helpful in understanding what AMSAT would really be up 
> against if it  wanted to have an independent GEO satellite or consider a 
> sub-GEO drifting orbit.

Thank you Ken, for the rocket scientist's take on it ;-)

It's refreshing to hear someone who actually has sat down and done the maths 
comment on how easy or hard it would be to put a satellite into a high orbit.

-- 
Gordon JC Pearce MM0YEQ 
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[amsat-bb] SatPc32 kepler Data

2011-10-11 Thread Howard Kowall
Hello all
I have an older laptop that has no internet connection,I run Satpc32 on my main 
computer that has internet connection and I am able to update the kepler data.I 
want to use the  kepler data from my main computer,and copy it to my laptop via 
USB  flash drive.I cant seem to find the kepler folder in the SatPc32 
folder.Has anyone one shared the kepler data.
Thanks to all who read and reply in advance
Howard
VE4ISP
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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Dave Marthouse
Question, what is the closest spacing for geo satellites to share the same
slot?  Is this theoretically practical and or possible?

Dave Marthouse N2AAM
dmartho...@gmail.com


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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Dave Marthouse
How about a high altitude drifter above the geo belt?  In fact wasn't that
talked about by a few amsat people in the early 80's.  I seem to remember
hearing it discussed by the late Rip WA2LQQ on the 75 meter Amsat net back
in the day.

Dave Marthouse N2AAM
dmartho...@gmail.com

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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Ken Ernandes
Paul -

Your final suggestion is something that is workable.  Placing a satellite say 
200 km below GEO would result in the satellite drifting about 10 minutes per 
day or about 2.5 degrees per day.  This would result in a cycle that repeats 
about every 144 days (or about 2.5 times per year), relative to a ground-based 
observer.  I'd need to see if 200 km is safe or if that might need to be 
increased.  An increase would correspondingly increase the drift rate.

As I said, that could be workable for an amateur satellite, but before the 
calls go out for this being AMSAT's next project we need to understand what 
we'd need to do, and what you'd actually be getting.

To get to such an orbit from a GTO would require about 950 m/sec of delta-V to 
raise perigee up and establish a nearly circular orbit, slightly below GEO.  If 
the propulsion system had 90% efficiency and we had a bi-propellant system with 
a 285 sec specific impulse (Isp), the propellant mass would be about 31.5% of 
the total spacecraft launch mass.  That is if we are willing to also accept the 
inclination that the launch booster dropped us off in.  I suspect we would 
accept the booster's inclination for reasons that we'll see.

Now I'd like to give a quick outline of the disturbing forces at GEO, since out 
spacecraft would experience similar effects.  

I'll start with what's commonly called Earth triaxiality.  Many of us know the 
Earth bulges at the equator.  So the first of the three axes is the Earth's 
rotational axis.  But the equator is not perfectly circular.  The equator 
itself has its own ellipsoidal shape, leading to two additional gravitational 
axes in the equatorial plane.  The result is that satellites on the GEO belt 
will tend to drift east or west (depending on location).  There are four 
equilibrium points, two of which are stable (about 75-deg E and 105-deg E) and 
two of which are not stable (about 12-deg W and 162-deg E).  The unstable 
points are the demarcations in which you will drift either east or west 
depending on which side of the that point you're located.  The stable points 
are the graveyards where all the dead satellites that haven't been boosted out 
of the GEO belt will collect.  The drift rate varies and is lowest near the 
equilibrium points and greatest at the mid-points between the equilibrium p!
 oints.  Given the case of a sub-GEO orbit, the drift due to triaxiality is of 
little consequence since the drift due to thee altitude difference is far 
greater and triaxiality would be reduced to a secondary effect.  It was 
provided here for understanding of what we would need to deal with if we wanted 
to hold at GEO and not collide with out neighbors.

A very significant effect results from the gravitational pulls on the satellite 
by the Sun and Moon.  (To be completely accurate, this is the difference 
between the pulls on the satellite and the Earth by these bodies.)  This causes 
the inclination to cycle between 0 and approximately 15-deg over a period of 
about 53 years.  Anybody familiar knows that inclination change maneuvers 
require a lot of propellant.  Thus, I believe we would accept this 
slowly-changing inclination and realize that our antennas would need to adjust 
slowly over the course of the day in what is typically a figure-8 pattern.  
Depending on your latitude, there may be periods when the satellite dips below 
your horizon.

A final effect to be considered is Solar Radiation Pressure.  The impact 
pressure from the Sun's photons impart momentum on the spacecraft, which in 
turn causes a slight change in velocity.  The main effect is a change to the 
orbital eccentricity.  For GEO satellites, eccentricity is manifest mainly by 
an east/west oscillation over the course of a day.  The larger the 
eccentricity, the greater the amplitude of the oscillation.  At first blush 
this may seem like an insignificant effect for out sub-GEO for the same reasons 
as we became unconcerned about triaxiality effects.  But eccentricity also 
equates to changes in altitude - precisely what we were using as our guard 
against colliding with satellites in the GEO belt.  So the long-term effects 
would need to be considered when choosing what we consider to be a safe 
separation from thee GEO belt.

I hope this is somehow helpful in understanding what AMSAT would really be up 
against if it  wanted to have an independent GEO satellite or consider a 
sub-GEO drifting orbit.

73, Ken Ernandes N2WWD

Sent from my iPad



On Oct 11, 2011, at 12:05 PM, Paul Williamson  wrote:

> On Oct 11, 2011, at 3:31 AM, Ken Ernandes wrote:
>> For those believing in the large space, small satellite theory, the risk of 
>> collision is more real than one might think.
> 
> It must be, since I would think the risk of collision is so tiny as to be 
> effectively negligible. If we position our satellite halfway between two of 
> those commercial "slots", we have a huge buffer on either side. Now I realize 
> that just mea

[amsat-bb] Re: KickSat - a personal spacecraft of your own in space

2011-10-11 Thread Trevor .
Hi Zac, 

I wish you well with the project it's a great idea.

I'd like to clarify the number of sprites that will be carried on the first 1U 
CubeSat. The website says: 

"KickSat is a CubeSat - a standardized small satellite that we can easily 
launch. It is designed to carry hundreds or even thousands of Sprites into 
space and deploy them in low Earth orbit."

Now looking at the picture showing the size of the boards for the initial 
deployment you aren't going to get 100's into a 1U CubeSat. How many will be 
deployed ?

I gather the Sprites have a very short lifetime, just days rather than months. 

Can you clarify the power level that will be used. Is it 10 milliwatts or lower 
? and is that power only available when the Sprite's solar panels are 
illuminated ?

73 Trevor M5AKA








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[amsat-bb] Re: geostationary satellite:thinking outside the box

2011-10-11 Thread andy thomas
I wonder if we could build a LEO uplinking to and downlinkingf rom a 
geosationary satellite on its spare transponder capacity? Initially by AX25 
packet from ground to the LEO sat on our frequencies, then by license up to the 
geo which would see the leo longer than a ground station would?
 
just my 1 penny worth...
 
73 de andy g0sfj
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[amsat-bb] Re: Geostationary Satellite

2011-10-11 Thread R Oler

I agree that the "best" hope for a GEO payload is a hosted one on a commercial 
sat, but the odds of it happening are pretty thin.

The biggest obstacle to this is not station keeping fuel however.  There are 
few satellites that simply run out of station keeping fuel with all their 
transponders working.  What ages a satellite is that the transponders start 
failing, the solar power system starts degrading...etc.  It simply IS NOT that 
they come up to the disposal fuel and thats it.

The biggest obstacle is integration of an amateur payload built by amateurs 
into something that has to work or there is a lot of money lost and there is no 
insurance recovery if something like an amateur payload caused the failure...or 
even some sort of problem with the primary payload.  

If AMSAT or anyone else could go for hosted payloads the best possible approach 
to that is some of the new intermediate altitude comm systems that are out 
there now looking for hosted payloads...

Robert G. Oler WB5MZO Life member AMSAT ARRL NARS

> From: howied...@hotmail.com
> To: amsat-bb@amsat.org
> Date: Tue, 11 Oct 2011 10:01:20 -0400
> Subject: [amsat-bb] Re: Geostationary Satellite
> 
> 
> I agree with much of what Dan, N8GFV, says. Our best hope of a high altitude 
> satellite is probably a hosted payload on a GEO sat. To make that viable we 
> need to consider the entire mission. GEO satellite operators are a for-profit 
> business and every aspect of a commercial satellite has a dollar value. The 
> major items are spectrum, power and fuel. Since hams bring their own 
> spectrum, that is a no cost item for us. If we need to use satellite power 
> then we would need to pay the market rate for the percentage of the total 
> satellite resource used for the design lifetime of the satellite, typically 
> 15 years. If the payload can be disabled by the operator we may be able to 
> negotiate a pay as you go plan so that we don't have to pre-pay 15 years 
> worth of power. Developing very power efficient transponder systems will 
> reduce our costs. Trading bandwidth for power by using digital encoding, 
> strong FEC, regenerative transponders with DSP signal enhancement will all 
> aid in the reduct!
 io!
>  n of the power required to close a link. 
> The other big cost factor is fuel. As previously stated here, station keeping 
> is a critical element in GEO satellites and with the advances of component 
> technology, a satellites lifetime in orbit is determined primarily by the 
> amount of station keeping fuel it can carry. The more fuel, the longer the 
> satellite life, the more time the operator can use to recover their 
> investment and make money. Every ounce added to the satellite affects the 
> cost of the launch and possibly the amount of fuel that can be carried on 
> board. Whether this is the case or not, the added satellite weight WILL add 
> to the launch cost that we would have to pay. 
> The good news is that the AMSAT community and the satellite operators have 
> common interests in making satellites less expensive and more efficient. By 
> building on the technology pioneered in ARISSAT-1 we MAY be able to get some 
> cooperation from a commercial operator to deploy a technology demonstration 
> package as a hosted payload. This might be more probable than one thinks. 
> Satellite operators are EXTREMELY conservative and don't deploy new 
> technology until it is thoroughly proven. The commercial satellite market is 
> running out of real estate. Many of the big operators are at over 80% 
> capacity. Since they are for-profit organizations, they are running out of 
> product quickly and will not be able to grow their business. All the major 
> operators are investing large amounts of money to promote a hosted payload 
> business where government and scientific users can bring their own bandwidth 
> to a transponder or payload on the operators platform. A low cost, high 
> performance, innovat!
 iv!
>  e payload COULD be a great advertising tool for a commercial operator. The 
> operator would get the payload for zero cost and could also get part of the 
> launch cost subsidized by AMSAT in return for a real world, open source 
> demonstration tool.
> If we build this payload along the lines of Tom Clark's C-C rider concept 
> with a 5 GHz up/ 3 GHz. down transponder we can probably even use the 
> satellites low gain telemetry antenna, further reducing payload costs.
> Sorry for the lengthy post but I have been thinking about this for a while 
> and this seemed like a good opportunity to finally put it in writing.
> HowieAB2S   
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[amsat-bb] % in EM55

2011-10-11 Thread wa4hfn

  The 5 in em55 award info can be seen on QRZ  lookup WA4NVM  or WA4HFN  . 
Skeds are ok too.
Several donations to AMSAT have been made from this award   Thank you

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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Bob Bruninga
>> the risk of collision is more real than one might think.

> I would think the risk of collision is so tiny 
> as to be effectively negligible.

I think it is, but when "negligible" incurs about a BILLION$$$ worth of
loss, it magnifies the risk.

> If we position our satellite halfway between two... "slots"

I think that is the problem.  One has to stay there.  GEO orbits are
impacted by the sun, moon and tides and solar wind.  All GEO orbits drift*.
Hence 90% of the mass of these GEO birds are fuel for station keeping.  And
that is where the risk comes from.  As soon as a spacecraft loses fuel, or
command/control, or any other problem that causes it to no longer keep its
station, it becomes a drifting hazard, moving literally FOREVER along this
extremely narrow orbit, the same orbit that all of these other satellites
are in!  It becomes a real hazard to them all.

That is why all nations now subscribe to the requirement that all GEO
spacecraft must have 10% reserve fuel to propel an aging satellite out to
the graveyard orbit.  And this must be done before there is loss of
command/control.

> Is there no clever trick of orbit design 
> that can be used to avoid collision? 

Not and be geostationary.  I think long term drift is the final state of any
GEO orbit.  Though there are , I think, *two spots on the entire GEO orcit
which are stable.. but guess what.  NO ONE WANTS them, because that is where
all the junk collects and that is where the chances of a collision with all
that junk is highest.

> We can even tolerate some long-term motion...
> Perhaps these extra freedoms would make it possible 
> to design an orbit that's close enough to geosynchronous 
> for our purposes, but far enough from the commercial orbits to be safe?

I'd guess that being in an orbit closer to earth would be best so that with
time we get further from the GEO arc.  But closer in, moves faster and so
all we have to do is chose the DRIFT rate.  Let it drift a full cycle once a
year, and the result is that any given country only sees it for 4  months a
year.  No matter where we put it, it will be out of view to any one station
2/3rds of the time.  But now that it is in its own special orbit, there wont
be any cheap rides to get there...

Our best bet is to piggy back on someone else's bird.

Oh, and it takes almost 10,000 times more power to hit a GEO bird at 22,500
miles away compared to hitting a LEO bird directly overhead (225 miles).

Just my 2 cents

Bob, Wb4APR

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[amsat-bb] WD9EWK @ Tucson AZ hamfest and post-hamfest activity, 22 October

2011-10-11 Thread Patrick STODDARD (WD9EWK/VA7EWK)
Hi!

The hamfest season out here in Arizona is about to start.  I will be
at the Old Pueblo Radio Club's annual hamfest in Tucson AZ a week from
Saturday, on 22 October 2011.  This is a week later than usual, since 
this hamfest has normally taken place the same weekend as the Scouting
Jamboree on the Air event.  The hamfest will be at the usual location
in Tucson, at the Kino Sports Complex along the north side of Ajo Way 
at Forgeus Avenue, east of the I-10 freeway and the baseball stadium 
(grid DM42me).  The hamfest officially runs from 7am-noon (1400-1900 
UTC), although people start showing up before sunrise and many leave 
before noon. 

During the hamfest, WD9EWK will be on whatever FM and SSB satellites
are available doing on-air demonstrations.  On the SSB birds, I try
to park about 5-10 kHz above the center of the transponders, depending
on other activity and QRM/QRN.  Please feel free to call WD9EWK during
those demonstrations and say "hello" to the crowds. 

After the hamfest, I plan on driving either to the DM51bx/DM52ba or 
DM52ax/DM53aa grid boundaries in southeastern Arizona to work some 
passes on my way home.  I have operated from both of these grid 
boundaries earlier this year - DM51bx/DM52ba in early May, and 
DM52ax/DM53aa in late March - and try to visit these locations when I 
attend hamfests in southern Arizona.  If you have a preference on which 
boundary I should try to work from after the hamfest, please e-mail me 
directly. I can't guarantee I will go to the spot you would prefer, but 
it helps to know what people are interested in hearing on the birds.  
As with the hamfest demonstrations, I am prepared to work both FM and 
SSB from wherever I go out there.  

As with my other trips away from the Phoenix area, there is no need
to send me a QSL request to get a WD9EWK QSL card for a hamfest QSO
or a QSO from one of those grid boundaries.  Just e-mail me the QSO
details - if you're in the log, you'll get a card.  QSOs will also
be uploaded to the Logbook of the World system as WD9EWK, including 
the grid(s) and county for each QSO.  

73!





Patrick WD9EWK/VA7EWK
http://www.wd9ewk.net/


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[amsat-bb] Re: KickSat - a personal spacecraft of your own in space

2011-10-11 Thread Zac Manchester
Hello All,

Sorry for taking so long to respond here on the AMSAT-BB - I know I've
spoken with some of you separately by email through kickstarter, but I
wanted to make sure I responded to everyone's concerns.

In response to Andreas' comments about wanting to use his own hardware
to listen to the Sprites, this is exactly the sort of thing I want to
encourage, and why I initially posted here.  I posted a brief "Amateur
Radio Information" item in the FAQ on kickstarter with some of this
information, but I'll try to cover everything here.

The Sprites will all be on the same frequency in the 70 cm band, and
each will use a unique PRN spreading code so they can be identified.
The hardware you'll need to receive these signals will be a yagi,
rotator, LNA, and software defined radio (SDR) interface.  We've been
using a USRP box from Ettus Research along with GNU Radio, but the
USRP is pretty expensive, so we're trying to make everything work with
the FUNCube dongle (http://www.funcubedongle.com/).  To work with the
FUNCube, we have to make sure the signal bandwidth is < 80 kHz (it's
currently around 100 kHz).  I'll be posting all the details of our
setup as we refine it, as well as all the code for the SDR.  Even if
you don't sponsor a Sprite, it would be great to have more people on
the ground listening in.  Everything we're doing will be documented,
open-sourced, and freely available online.

We will most definitely abide by all regulations and apply for
frequency coordination with the IARU.  We haven't taken that step yet
because we have to actually be slotted for a specific launch first.
This is also why we don't know our exact frequency yet.

Please let me know if you have any additional questions.

Thanks,
Zac
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[amsat-bb] Re: Am-Comm Clear Speech Base DSP Filter For Sale

2011-10-11 Thread Alan P. Biddle
The unit has been taken.  Thanks to those who inquired.

73s,

Alan
WA4SCA
 

-Original Message-
From: amsat-bb-boun...@amsat.org [mailto:amsat-bb-boun...@amsat.org] On
Behalf Of Alan P. Biddle
Sent: Monday, October 10, 2011 3:33 PM
To: AMSAT-BB
Subject: [amsat-bb] Am-Comm Clear Speech Base DSP Filter For Sale

I am doing some shack cleaning.

This unit was originally sold by Am-Comm. Since then, the basic electronics
have been repackaged, sometimes combined with a speaker, and sold by various
companies. My experience is that most of the time it is amazing, though
rarely it does very little. The exact improvement depends on the signal,
type of noise, levels, etc.  It made the difference on AO-40 around apogee.

http://www.eham.net/reviews/detail/1041

Currently West Mountain Radio is selling a similar unit, with an adjustable
threshold added:

http://www.westmountainradio.com/product_info.php?products_id=clr_dsp

The unit is perfect mechanically and electrically.  $80 including shipping
in North America.  

Please contact me off list.

Alan
WA4SCA




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[amsat-bb] Fwd: Satellite Beacon Tracking Request

2011-10-11 Thread Mani VU2WMY

Dear friends,
As you all might be aware that two cubesats 'Jugnu' and 'SRMSat' using  
amateur frequencies are to be launched by PSLV C-18 from Satish Dhawan  
Space Centre [SDSC], Shriharikota, India. The expected launch time is  
05:30 UT.


In this regard, I'm herewith forwarding the mail from Mr. Shantanu  
Agarwal, Team Lead for the 'Jugnu', requesting the Global Amateur  
Radio fraternity to provide the CW Beacon signal Report along with the  
plain decoded morse message, if possible.


Any help in this regard would be greatly appreciated, as this would be  
very helpful to evaluate various ob-board system performance.


'Jugnu' beacon is at 437.275 MHz, OOK.

The reports can be sent to the following mail ID.s
w...@isac.gov.in
shan...@iitk.ac.in

The predicted TLE's:

JNU
1 9U 11072A   11285.2472  .1785  0-0  96625-3 0  1235
2 9  20.0506  66.7109 0018405   5.1080 190.7439 14.1133892219
SRM
1 8U 11072A   11278.34967500  .1077  0-0  60876-3 0  1233
2 8  20.0603  97.4017 0010015 338.6461 208.4324 14.0919996814


 Thanks in advance and looking forward to your valuable reports.

73 de

Mani, VU2WMY
Secretary & Station-In-Charge
Upagrah Amateur Radio Club VU2URC
ISRO Satellite Centre
HAL Airport Road, Bangalore-560 017.
Phone:(O)91-80-25082054/2598/2192
Mobile:  91-80-98803 41456
E-mail ID: w...@isac.gov.in
   vu2wmy_m...@yahoo.com
   isroh...@yahoo.com

- Forwarded message from shan...@iitk.ac.in -
Date: Tue, 11 Oct 2011 20:06:56 +0530
From: Shantanu 
 Subject: Satellite Beacon Tracking Request
  To: w...@isac.gov.in

Dear Sir,

We will be thankful if you can track our satellite beacon after launch.

You are requested to kindly post our satellite details on various HAM
groups to track our satellite beacon after launch.

Our satellite beacon is at 437.275 MHz, OOK.

Thanks.
Shantanu Agarwal



- End forwarded message -




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contact the sender by reply e-mail and destroy all copies of the original
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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Paul Williamson
On Oct 11, 2011, at 3:31 AM, Ken Ernandes wrote:
> For those believing in the large space, small satellite theory, the risk of 
> collision is more real than one might think.

It must be, since I would think the risk of collision is so tiny as to be 
effectively negligible. If we position our satellite halfway between two of 
those commercial "slots", we have a huge buffer on either side. Now I realize 
that just measuring distances doesn't capture the whole story, and that orbital 
dynamics can be non-intuitive, but it boggles the mind that objects spaced that 
far apart can't be kept from colliding without extraordinary measures. 

I would say that I'd like to see the analysis to back up the worry, but I doubt 
I'd understand it. You would, though, so I can only ask whether you have seen 
the actual analysis and found it compelling.

Is there no clever trick of orbit design that can be used to avoid collision? 
We can afford bigger position errors than the commercial guys can, because we 
have smaller ground station antennas and no problem with interference crowding. 
We can even tolerate some long-term motion, since we can certainly accept an 
occasional adjustment to each ground station. Perhaps these extra freedoms 
would make it possible to design an orbit that's close enough to geosynchronous 
for our purposes, but far enough from the commercial orbits to be safe?

73  -Paul
kb...@amsat.org


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[amsat-bb] Re: Geostationary Satellite

2011-10-11 Thread Andre

Op 11-10-2011 16:23, Joe schreef:
Too bad we can't get one of the TV sat people to allow us to have one 
of their channels.  It would be wide enough to hold hundreds of QSO's 
at the same time for sure.  And I bet they have at least one that 
isn't doing anything at all.


But of course thats not a ham band either  bummer!

Joe WB9SBD

The Original Rolling Ball Clock
Idle Tyme
Idle-Tyme.com
http://www.idle-tyme.com
That has been done in the 90's upto december 2001, the dutch ATV relay 
PI6ALK had a digital stream on Astra 1 satelite using a demonstation 
transponder.
In the end it was not the transponder that caused the end of this 
experiment but the cost of running the uplink station.


73 Andre PE1RDW
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[amsat-bb] 2011 AMSAT Space Symposium Hotel Reservations

2011-10-11 Thread Martha
People - I have contacted the Wyndham hotel in San Jose CA and they have
agreed to move the cutoff date for room reservations to *October 24th*. The
phone number is 408-453-6200 and the reservation block code is AMSAT.  The
Symposium is November 4th - 6th with an optional tour on Sunday.  For more
information, go to the AMSAT website.  Don't forget to register for the
meeting and the banquet at the AMSAT store found on the website.

-- 
73- Martha
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[amsat-bb] Re: Geostationary Satellite

2011-10-11 Thread Tom Schaefer, NY4I
I ask this in all seriousness though. Is a giant repeater in the sky with no 
need to handle Doppler shift really something that would be used? That would 
take some of the magic out of it. Having to follow a schedule and have the 
computer and radio synced to correct for the shift is part of the operating 
fun. Sure we hear some of the same people but it is the station that pops in on 
the low elevation passes that make it special. 

This seems like the same idea of explaining to a "hamshack on the belt" type 
the magic of HF. Yes, you have to check the propagation and MUF. What is the 
best band to talk on. All the things that lead to making contacts with 
different places on HF. While it would be nice to push up North American VUCC 
numbers, I just don't see why anyone would want a geo-stationary satellite for 
ham activities. I can guarantee at least two of my friends are on the local 
repeater right now. That is great if I have to get ahold of them for something 
or if I am on the side of the road in a ditch (although the auto club on my 
cell phone is my preferred mode of choice in that situation). 

Due to the costs, the is clearly academic, but as we frequently hear rumblings 
of a GEOSYNC bird (from me too in the past), when I really look at why I like 
operating satellites, that type of bird would have none of that. 

I am glad someone brought this up though as it caused me to re-examine my own 
beliefs about it.

Thanks,


Tom Schaefer, NY4I
n...@arrl.net
EL88pb 
Monitoring EchoLink node KJ4FEC-L 489389
DSTAR Capable  APRS: NY4I-15



On Oct 11, 2011, at 10:23 AM, Joe wrote:

> Too bad we can't get one of the TV sat people to allow us to have one of 
> their channels.  It would be wide enough to hold hundreds of QSO's at the 
> same time for sure.  And I bet they have at least one that isn't doing 
> anything at all.
> 
> But of course thats not a ham band either  bummer!
> 
> Joe WB9SBD
> 
> The Original Rolling Ball Clock
> Idle Tyme
> Idle-Tyme.com
> http://www.idle-tyme.com
> 
> On 10/11/2011 9:01 AM, Howie DeFelice wrote:
>> I agree with much of what Dan, N8GFV, says. Our best hope of a high altitude 
>> satellite is probably a hosted payload on a GEO sat. To make that viable we 
>> need to consider the entire mission. GEO satellite operators are a 
>> for-profit business and every aspect of a commercial satellite has a dollar 
>> value. The major items are spectrum, power and fuel. Since hams bring their 
>> own spectrum, that is a no cost item for us. If we need to use satellite 
>> power then we would need to pay the market rate for the percentage of the 
>> total satellite resource used for the design lifetime of the satellite, 
>> typically 15 years. If the payload can be disabled by the operator we may be 
>> able to negotiate a pay as you go plan so that we don't have to pre-pay 15 
>> years worth of power. Developing very power efficient transponder systems 
>> will reduce our costs. Trading bandwidth for power by using digital 
>> encoding, strong FEC, regenerative transponders with DSP signal enhancement 
>> will all aid in the reduc!
 t!
> io!
>>  n of the power required to close a link.
>> The other big cost factor is fuel. As previously stated here, station 
>> keeping is a critical element in GEO satellites and with the advances of 
>> component technology, a satellites lifetime in orbit is determined primarily 
>> by the amount of station keeping fuel it can carry. The more fuel, the 
>> longer the satellite life, the more time the operator can use to recover 
>> their investment and make money. Every ounce added to the satellite affects 
>> the cost of the launch and possibly the amount of fuel that can be carried 
>> on board. Whether this is the case or not, the added satellite weight WILL 
>> add to the launch cost that we would have to pay.
>> The good news is that the AMSAT community and the satellite operators have 
>> common interests in making satellites less expensive and more efficient. By 
>> building on the technology pioneered in ARISSAT-1 we MAY be able to get some 
>> cooperation from a commercial operator to deploy a technology demonstration 
>> package as a hosted payload. This might be more probable than one thinks. 
>> Satellite operators are EXTREMELY conservative and don't deploy new 
>> technology until it is thoroughly proven. The commercial satellite market is 
>> running out of real estate. Many of the big operators are at over 80% 
>> capacity. Since they are for-profit organizations, they are running out of 
>> product quickly and will not be able to grow their business. All the major 
>> operators are investing large amounts of money to promote a hosted payload 
>> business where government and scientific users can bring their own bandwidth 
>> to a transponder or payload on the operators platform. A low cost, high 
>> performance, innova!
 t!
> iv!
>>  e payload COULD be a great advertising tool for a commercial operator. The 
>> operator would g

[amsat-bb] Re: Geostationary Satellite

2011-10-11 Thread Joe
Too bad we can't get one of the TV sat people to allow us to have one of 
their channels.  It would be wide enough to hold hundreds of QSO's at 
the same time for sure.  And I bet they have at least one that isn't 
doing anything at all.


But of course thats not a ham band either  bummer!

Joe WB9SBD

The Original Rolling Ball Clock
Idle Tyme
Idle-Tyme.com
http://www.idle-tyme.com

On 10/11/2011 9:01 AM, Howie DeFelice wrote:

I agree with much of what Dan, N8GFV, says. Our best hope of a high altitude 
satellite is probably a hosted payload on a GEO sat. To make that viable we 
need to consider the entire mission. GEO satellite operators are a for-profit 
business and every aspect of a commercial satellite has a dollar value. The 
major items are spectrum, power and fuel. Since hams bring their own spectrum, 
that is a no cost item for us. If we need to use satellite power then we would 
need to pay the market rate for the percentage of the total satellite resource 
used for the design lifetime of the satellite, typically 15 years. If the 
payload can be disabled by the operator we may be able to negotiate a pay as 
you go plan so that we don't have to pre-pay 15 years worth of power. 
Developing very power efficient transponder systems will reduce our costs. 
Trading bandwidth for power by using digital encoding, strong FEC, regenerative 
transponders with DSP signal enhancement will all aid in the reduct!

io!

  n of the power required to close a link.
The other big cost factor is fuel. As previously stated here, station keeping 
is a critical element in GEO satellites and with the advances of component 
technology, a satellites lifetime in orbit is determined primarily by the 
amount of station keeping fuel it can carry. The more fuel, the longer the 
satellite life, the more time the operator can use to recover their investment 
and make money. Every ounce added to the satellite affects the cost of the 
launch and possibly the amount of fuel that can be carried on board. Whether 
this is the case or not, the added satellite weight WILL add to the launch cost 
that we would have to pay.
The good news is that the AMSAT community and the satellite operators have 
common interests in making satellites less expensive and more efficient. By 
building on the technology pioneered in ARISSAT-1 we MAY be able to get some 
cooperation from a commercial operator to deploy a technology demonstration 
package as a hosted payload. This might be more probable than one thinks. 
Satellite operators are EXTREMELY conservative and don't deploy new technology 
until it is thoroughly proven. The commercial satellite market is running out 
of real estate. Many of the big operators are at over 80% capacity. Since they 
are for-profit organizations, they are running out of product quickly and will 
not be able to grow their business. All the major operators are investing large 
amounts of money to promote a hosted payload business where government and 
scientific users can bring their own bandwidth to a transponder or payload on 
the operators platform. A low cost, high performance, innovat!

iv!

  e payload COULD be a great advertising tool for a commercial operator. The 
operator would get the payload for zero cost and could also get part of the 
launch cost subsidized by AMSAT in return for a real world, open source 
demonstration tool.
If we build this payload along the lines of Tom Clark's C-C rider concept with 
a 5 GHz up/ 3 GHz. down transponder we can probably even use the satellites low 
gain telemetry antenna, further reducing payload costs.
Sorry for the lengthy post but I have been thinking about this for a while and 
this seemed like a good opportunity to finally put it in writing.
HowieAB2S   
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[amsat-bb] Re: Geostationary Satellite

2011-10-11 Thread Howie DeFelice

I agree with much of what Dan, N8GFV, says. Our best hope of a high altitude 
satellite is probably a hosted payload on a GEO sat. To make that viable we 
need to consider the entire mission. GEO satellite operators are a for-profit 
business and every aspect of a commercial satellite has a dollar value. The 
major items are spectrum, power and fuel. Since hams bring their own spectrum, 
that is a no cost item for us. If we need to use satellite power then we would 
need to pay the market rate for the percentage of the total satellite resource 
used for the design lifetime of the satellite, typically 15 years. If the 
payload can be disabled by the operator we may be able to negotiate a pay as 
you go plan so that we don't have to pre-pay 15 years worth of power. 
Developing very power efficient transponder systems will reduce our costs. 
Trading bandwidth for power by using digital encoding, strong FEC, regenerative 
transponders with DSP signal enhancement will all aid in the reductio!
 n of the power required to close a link. 
The other big cost factor is fuel. As previously stated here, station keeping 
is a critical element in GEO satellites and with the advances of component 
technology, a satellites lifetime in orbit is determined primarily by the 
amount of station keeping fuel it can carry. The more fuel, the longer the 
satellite life, the more time the operator can use to recover their investment 
and make money. Every ounce added to the satellite affects the cost of the 
launch and possibly the amount of fuel that can be carried on board. Whether 
this is the case or not, the added satellite weight WILL add to the launch cost 
that we would have to pay. 
The good news is that the AMSAT community and the satellite operators have 
common interests in making satellites less expensive and more efficient. By 
building on the technology pioneered in ARISSAT-1 we MAY be able to get some 
cooperation from a commercial operator to deploy a technology demonstration 
package as a hosted payload. This might be more probable than one thinks. 
Satellite operators are EXTREMELY conservative and don't deploy new technology 
until it is thoroughly proven. The commercial satellite market is running out 
of real estate. Many of the big operators are at over 80% capacity. Since they 
are for-profit organizations, they are running out of product quickly and will 
not be able to grow their business. All the major operators are investing large 
amounts of money to promote a hosted payload business where government and 
scientific users can bring their own bandwidth to a transponder or payload on 
the operators platform. A low cost, high performance, innovativ!
 e payload COULD be a great advertising tool for a commercial operator. The 
operator would get the payload for zero cost and could also get part of the 
launch cost subsidized by AMSAT in return for a real world, open source 
demonstration tool.
If we build this payload along the lines of Tom Clark's C-C rider concept with 
a 5 GHz up/ 3 GHz. down transponder we can probably even use the satellites low 
gain telemetry antenna, further reducing payload costs.
Sorry for the lengthy post but I have been thinking about this for a while and 
this seemed like a good opportunity to finally put it in writing.
HowieAB2S 
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[amsat-bb] Re: Geostationary Satellites

2011-10-11 Thread Ken Ernandes
You are viewing it only from the point of view of signal interference.  In 
reality, the greater issue is maintaining our position and the risk of 
collision.  There is a very tight band that defines geostationary and there are 
some significant disturbing forces: Earth's triaxial gravity distribution, 
lunar and solar gravity, and solar radiation pressure.  This mandates that 
there be vigilance in monitoring the satellite's orbit and those of its 
neighbors and to also have a propulsion system capable of station-keeping on a 
regular basis.  Even without the risk of collision, not holding the position 
tightly nullifies the benefit of fixed antenna pointing.

For those believing in the large space, small satellite theory, the risk of 
collision is more real than one might think.  I could only imagine the 
legislation and regulations that might be placed on amateur satellites if we 
failed to control our bird and it collided with a very expensive commercial or 
government asset.  Until AMSAT can build enough experience to operate a 
propulsion system reliably for the long term, I don't think we can responsibly 
operate a satellite bus on a congested orbital highway.

73, Ken N2WWD

Sent from my iPad



On Oct 10, 2011, at 10:59 PM, Paul Williamson  wrote:

> On Oct 10, 2011, at 3:03 PM, Ken Ernandes wrote:
>> 1.  There are a finite number of orbital slots at Geostationary.  That is 
>> essentially like water front property.  
> 
> I've heard that asserted before, but I question the reasoning.
> 
> My understanding is that spacing of satellites around the geostationary orbit 
> is dictated by the beamwidth of the ground station antennas. In other words, 
> it's a matter of spatial frequency sharing. The satellites have to be far 
> enough apart that a ground station antenna can illuminate one of them without 
> causing too much harmful interference to the ones in the adjacent slots, 
> after all the expected errors (orbital and ground station pointing) are taken 
> into account.
> 
> If that's correct, since amateur radio satellite operate on different 
> frequencies from the commercial satellites, there is no conflict between 
> amateur radio satellites and commercial satellites for orbital slots.
> 
> Where have I gone wrong?
> 
> 73  -Paul
> kb...@amsat.org
> 

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