[amsat-bb] Re: HEO Arsene AO-24

2011-02-04 Thread John B. Stephensen
I was thinking of the mode S linear transponder portion of the satellite. It 
had a narrow passband and produced about 1 watt. You needed a 4-6 foot dish 
for the downlink. Since a 3U cubesat can generate about 6 W of DC power with 
solar panels and the largest surface for mounting antennas is 11.5 x 3.5, 
this would be the kind of satellite that we could expect for an $800k launch 
cost.

73,

John
KD6OZH

- Original Message - 
From: f6...@aol.com
To: amsat-bb@amsat.org
Sent: Friday, February 04, 2011 15:44 UTC
Subject: [amsat-bb] HEO Arsene AO-24



 Here is a detailed description from the past (sorry found only in French)

 http://www.amsat-france.org/spipamsat/IMG/pdf/Descriptif_ARSENE.pdf

 and photos:

 http://www.amsat-france.org/spipamsat/article.php3?id_article=61


 73 de Michel F6HTJ



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[amsat-bb] Re: Rideshare missions to GTO, $800K for 3U Cubesat

2011-02-03 Thread John B. Stephensen
The interesting question is is how much will AMSAT members be willing to 
invest in ground stations. A 3U cubesat could provide a HEO satellite 
similar to Arsene (AO-24).

73,

John
KD6OZH

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[amsat-bb] Re: Any update on P3E?

2010-05-16 Thread John B. Stephensen
I don't think that it is due to ITAR as there are enough Europeans available 
to complete the satellite. AMSAT-DL is trying to get government funding for 
the Mars mission (P5A) for which P3E will be a testbed. They haven't made 
any announcement about securing funding and now the EU appears to be in 
worse financial shape than the US.

73,

John
KD6OZH

- Original Message - 
From: Mike sar...@bellsouth.net
To: AMSAT-BB@amsat.org
Sent: Sunday, May 16, 2010 20:07 UTC
Subject: [amsat-bb] Re: Any update on P3E?


P3 as I understand it if back shelved for now due to ITAR issues.

-Original Message-
From: amsat-bb-boun...@amsat.org [mailto:amsat-bb-boun...@amsat.org] On
Behalf Of Peter Sils
Sent: Sunday, May 16, 2010 3:39 PM
To: amsat-bb@amsat.org
Subject: [amsat-bb] Any update on P3E?

I am wondering if there is any update to the status of P3E?

I have not seen any mention of it for a long time and wondering if it is
built and ready to launch or has the project been put on hold because of
launch expenses?

Any update would be appreciated!

73 Peter
KD0AA



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[amsat-bb] Re: BeeSat at 4800 GMSK

2010-04-06 Thread John B. Stephensen
Symek sells modems that can be modified for operation at 4.8-614.4 kbaud 
(http://www.symek.com/g/index-g.html).

73,

John
KD6OZH

- Original Message - 
From: Nathaniel S. Parsons ns...@cornell.edu
To: AMSAT-BB amsat-bb@amsat.org
Sent: Tuesday, April 06, 2010 16:40 UTC
Subject: [amsat-bb] BeeSat at 4800 GMSK


 Hi all,

 I didn't get a response the last time I asked, so I'll try again, slightly
 differently.

 What TNC or TNC-like equipment do I need to listen to BeeSat at 4800 bps? 
 I
 have a TS-2000, yagi antenna, rotator, and KAM-XL, but the KAM-XL can only
 do GMSK at 9600 bps.

 Thanks in advance for your time,

 Nate KC2SVI
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[amsat-bb] Re: seeking examples of frequency bands used in amateurspacecraft

2010-04-06 Thread John B. Stephensen
The RS (radio sputnik) series used the 10 and 15 m bands but no other HF 
bands were used as far as I know. Various OSCARs used freqencies between 28 
MHz and 47 GHz with the exception of the 3.4 GHz band. 29.3-29.5 MHz, 
145.8-146 and 435-438 MHz were generally used but AO-13 and some of the 
PACSATs added use of 1260-1270 MHz and 2400-2450 MHz. The rest only appeared 
in AO-40.

73,

John
KD6OZH

- Original Message - 
From: Samudra Haque samudra.ha...@gmail.com
To: Amsat-bb amsat-bb@amsat.org
Sent: Tuesday, April 06, 2010 19:03 UTC
Subject: [amsat-bb] seeking examples of frequency bands used in 
amateurspacecraft


 Hello with reference to the US FCC Part 97 and in particular section 
 97.207
 Space Station available
 http://www.arrl.org/FandES/field/regulations/news/part97/c.html#207

 Have all of the frequency bands listed below been used in service through
 the last four decades?

 The following frequency bands and segments are authorized to space 
 stations:



   (1) The 17 m, 15 m, 12 m and 10 m bands, 6 mm, 4 mm, 2 mm and 1 mm 
 bands;
   and

   (2) The 7.0-7.1 MHz, 14.00-14.25 MHz, 144-146 MHz, 435-438 MHz, 
 1260-1270
   MHz and 2400-2450 MHz, 3.40-3.41 GHz, 5.83-5.85 GHz, 10.45-10.50 GHz and
   24.00-24.05 GHz segments.



 What power limitations are stipulated for these bands?


 Samudra, N3RDX  S21X
 Alexandria, VA
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[amsat-bb] Re: Winter Project

2010-01-10 Thread John B. Stephensen
Try the ARRL Periodicals Archive search. There were a lot of construction 
articles published in the 1950's and 1960's that can be downloaded at no 
charge. RF Parts and Surplus Sales of Nebraska stock parts.

Remember to keep one hand in your pocket when troubleshooting. If you give 
the high voltage a path to ground through your heart, you're dead.

73,

John
KD6OZH

 - Original Message - 
 From: Douglas Anoman dano...@email.itt-tech.edu
 To: amsat-bb@amsat.org
 Sent: Thursday, January 7, 2010 7:56:29 AM GMT -08:00 US/Canada Pacific
 Subject: [amsat-bb] Winter Project


 I'm looking for a winter project can any one point me in the direction of 
 a 2 meter tube amp nothing crazy about 25-50 out, 1-10 in. I have never 
 used or played with a tube circuit so i thougt winter why not. Thanks 73

 Thank You
 Douglas Anoman
 KC9MLN
 kc9...@amsat.org
 Amsat #37043

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[amsat-bb] Re: Eagle P3E status?

2009-12-22 Thread John B. Stephensen
There in no launch date for either. There are no more inexpensive launches 
available from ESA so the AMSATs are trying to get non-amateur funding to 
pay for HEO launches. Assume LEO satellites for the next few years as launch 
costs are much lower. CAMSAT just launched one, AMSAT-NA plans on launching 
two and there are others in the works.

73

John
KD6OZH

- Original Message - 
From: KG0MW-Chad Phillips kg...@greatplainsphotography.com
To: AMSAT-BB@amsat.org
Sent: Tuesday, December 22, 2009 03:29 UTC
Subject: [amsat-bb] Eagle  P3E status?


 Just wondering if anyone has the thread about the status of P3E and
 Eagle. I have been away for six years and am rebuilding the station
 now. Just trying to figure out what gear to build for what birds.
 Thanks in advance,
 Chad
 kg0mw - EN13

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[amsat-bb] Re: Satellites need to be open source

2009-11-13 Thread John B. Stephensen
Since you are in Canada you don't have to worry about U.S. laws.

73,

John
KD6OZH

- Original Message - 
From: Luc Leblanc luclebla...@videotron.ca
To: amsat-bb@amsat.org
Cc: eu-am...@yahoogroups.com
Sent: Friday, November 13, 2009 07:54 UTC
Subject: [amsat-bb] Re: Satellites need to be open source


 On 12 Nov 2009 at 13:02, Clint Bradford wrote:

 Date sent:  Thu, 12 Nov 2009 13:02:58 -0800
 From:   Clint Bradford clintbra...@earthlink.net
 Subject:[amsat-bb] Re: Satellites need to be open source
 To: amsat-bb@amsat.org

   ... Why aren't the schematics ... posted on the internet?


 I think the info IS out there. AMSAT-NA doesn't seem to be hiding
 anything.

 If all is publicly open how ITAR seems to prevent disclosure of the very 
 same technology used by AMSAT-NA or anyone else! there is already
 know SDR and others widely available technology very well documented

 It will be useful to see the papers issued by ITAR afficionados against 
 AMSAT-NA to see what they have made wrong and against ITAR rules?
 They surely pointed out some inappropriate actions and the disclosure of 
 theses inappropriate actions will help a lot of us as many are
 already transferring notes schematic data files and so on in a way to 
 share satellite technology between ham's.

 I already received some request about DSTAR coding and DSTAR technology 
 information from some universities and i'm exchanging files on the
 very same subject with europe can i violate ITAR or those in the US who 
 send me some files are they violating ITAR?

 I got at a hamfest a special transmitter who was supposed to be a very 
 wide VHF transmitter but the output is made only of white noise
 with hissing special effect... as usual i come up with the first 
 conclusion that i got another piece of scrap but pushing a bit more my
 search i found it was an exciter part of a power chain apparently made on 
 purpose to transmit only noise... be my guess what the primary
 use of this transmitter was but how many of us can stumble on some weird 
 piece of equipment and when making theses items available for swap
 of for sale did we violate ITAR?

 The disclosure of the ITAR rules apparently violated by AMSAT-NA will only 
 help us to see if we are on the right track or on the side one.

 P.S. i got a Power Supply who come up with my unmark noise transmiter it 
 is a Qualidyne switching power supply model 9010E-1Z-001 SN: 70121
 it is rated for 1200Watts 12V at 100amps if any one can help me finding at 
 least the schematic in a way to find how to switch it on. Only
 the fan start when i plugged it into the AC main.

 Thank's

 -


 Luc Leblanc VE2DWE
 Skype VE2DWE
 www.qsl.net/ve2dwe
 DSTAR urcall VE2DWE
 WAC BASIC CW PHONE SATELLITE



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[amsat-bb] Re: Why do hamsats? (Or anything else...)

2009-10-18 Thread John B. Stephensen
Suitsat 2/ARISSsat is a linear transponder done with DSP. Its seems 
perfectly reasonable to me to do transponder signal filtering and command 
decoding digitally as it makes things smaller and lighter. You could also 
make a better transponder by forming filters around the uplink signals so 
downlink power isn't wasted by repeating noise and downlink power could be 
allocated equally among users.

Putting ARISSsat on the ISS would be nice but NASA and the Russian space 
agency haven't agreed to that.

73,

John
KD6OZH

- Original Message - 
From: Rocky Jones orbit...@hotmail.com
To: k...@arrl.net; Amsat BB amsat-bb@amsat.org
Sent: Sunday, October 18, 2009 15:32 UTC
Subject: [amsat-bb] Re: Why do hamsats? (Or anything else...)


 That still doesnt answer the question of why on Suitsat 2 they should fly 
 a digital transponder.

 In my view better engineering doctrine would imply that we try and put the 
 digital transponder ON ISS and let it cook there for a bit.
 Robert WB5MZO


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[amsat-bb] Re: According to Rocky Jones

2009-10-18 Thread John B. Stephensen
Your math seems to be off. Eagle disappeared due to lack of money to pay for 
a launch rather than technical problems. This is much better than paying for 
hardware to sit on the ground. Suitsat 2 and ARRISsat are the same thing so 
there has been no failure yet.AO-51 is in orbit and working.

73,

John
KD6OZH

- Original Message - 
From: Rocky Jones orbit...@hotmail.com
To: ni...@ngunn.net
Cc: Amsat BB amsat-bb@amsat.org
Sent: Sunday, October 18, 2009 15:49 UTC
Subject: [amsat-bb] Re: According to Rocky Jones





 Date: Sun, 18 Oct 2009 15:44:57 +
 From: ni...@ngunn.net
 To: orbit...@hotmail.com
 CC: amsat-bb@amsat.org
 Subject: According to Rocky Jones

 I guesswe need to get you on the design/construction team to show the 
 experts how to do it.



 the experts were very successful with Suitsat 1.  Eagle worked out good as 
 well didnt it?

 Suitsat 2...dellivered on time ...oh well not so much.  ARISSsat or 
 whatever it is...fourth time is a charm

 Robert WB5MZO

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[amsat-bb] Re: THE DMSP launch

2009-10-18 Thread John B. Stephensen
Do you think that they would agree to fly anything other than ballast? Have 
you talked to the project manager? AMSAT has flown satellites using excess 
space in the past because the launch agency agreed years in advance and the 
satellites were built to fit in that space.

73,

John
KD6OZH

- Original Message - 
From: Rocky Jones orbit...@hotmail.com
To: Rocky Jones orbit...@hotmail.com
Cc: Amsat BB amsat-bb@amsat.org
Sent: Sunday, October 18, 2009 17:12 UTC
Subject: [amsat-bb] THE DMSP launch



 We have a unique opportunity with the Atlas 5/DMSP launch, as DMSP is
 a relatively lighter spacecraft than many of those that fly on Atlas.
 For that reason, we have a tremendous amount of performance margin.
 That's certainly not the case for some future missions that Atlas will
 be flying. So we're taking advantage of the opportunity before us to
 use some of that excess performance margin on the Atlas 5, said Col.
 Michael Moran, the Atlas Group commander.

 to bad we didnt have something to use that excess performance...they flew 
 ballast on the flight

 Robert WB5MZO

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[amsat-bb] Re: AMSAT Symposium News Posted to the Web

2009-10-14 Thread John B. Stephensen
AMSAT has a U/V linear transponder design in ARISSsat and according to the 
last newsletter no foreign national has signed the agreement that ITAR 
requires.

73,

John
KD6OZH

- Original Message - 
From: Rocky Jones orbit...@hotmail.com
To: n...@bellsouth.net; luclebla...@videotron.ca; Amsat BB 
amsat-bb@amsat.org
Sent: Wednesday, October 14, 2009 15:58 UTC
Subject: [amsat-bb] Re: AMSAT Symposium News Posted to the Web



http://www.qsl.net/pe1rah/HAMSAT.htm

I am just trying to figure out why AMSAT NA is not taking advantage of work 
already done.

Robert WB5MZO

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[amsat-bb] Re: Understanding ITAR

2009-10-04 Thread John B. Stephensen
One purpose of ITAR is preventing technological advances useful to our 
military (including satellites) from getting into enemy hands. Security 
people always want regulations to be as broad as possible. Even if 99% of 
the technology is available elsewhere they want it examined in order to 
catch the 1% that could be a problem.

73,

John
KD6OZH

- Original Message - 
From: Bill Ress b...@hsmicrowave.com
To: Wayne Estes w...@charter.net
Cc: amsat-bb@amsat.org
Sent: Saturday, October 03, 2009 22:03 UTC
Subject: [amsat-bb] Re: Understanding ITAR


 Hi Wayne,

 The State Department defines what is considered a munition in the ITAR
 regulations. See: http://pmddtc.state.gov/

 The criteria is obviously determined by the State Department with
 direction from the Congress. The article just tries to describe some
 examples without trying to justify or explain why something is or isn't
 a munition.

 The main point of the article is that any communications satellite,
 whether it is an Amateur, a university or a commercial satellite is
 considered by ITAR to be a munition controlled by ITAR export
 regulations. That's a fact and to understand the criteria is to
 understand the thinking of the authors of the regulation (State
 Department and the Congress), which I can't do.

 To be sure, export regulations can be complicated and at times appear to
 us as being irrational. But the fact remains, ITAR is an export law that
 we at AMSAT have to comply with.

 Regards...Bil - N6GHz

 Wayne Estes wrote:
 I just read the article about ITAR in the Jan/Feb 2009 AMSAT Journal.  I
 have to say that the article didn't help me understand ITAR at all.  It
 seems to have skipped the first several steps in the explanation.

 For example, what criteria are used to judge that a device has dual use
 as a munition?  It is not at all obvious to my feeble mind how a 23 GHz
 amplifier or IHU-3 (computer) can be judged to have dual use as a 
 munition.

 What criteria does ITAR law use to EXCLUDE devices that have obvious
 dual uses as munitions?  For example, GSM cell phones have been used to
 remotely control explosive devices that killed thousands of U.S.
 servicemen.  Are they not regulated because they are too ubiquitous to
 control?

 Wayne Estes W9AE
 Oakland, Oregon, USA, CN83ik
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[amsat-bb] Re: All Satellites (Alan P. Biddle)

2009-09-28 Thread John B. Stephensen
FDMDV uses a 1400 bps codec, occupies only 1100 Hz and operates with any SSB 
transceiver. Comunications doesn't have to be full duplex. At 12-16 kbps the 
satellite and ground stations could alternate with short bursts of voice or 
text. This wouldn't fit in a 2.4 kHz SSB bandwidth but would require a 16-20 
kHz wide filter or use of a transverter and a simple SDR radio like the 
SoftRock.

73,

John
KD6OZH

- Original Message - 
From: Gordon JC Pearce gordon...@gjcp.net

 KD6OZH's mentioning of a 1200 bps voice codec is very interesting,
 too. I see that DSTAR's AMBE is down to 2000  with error correction,
 and Speex operates down to 2000, too, though I think without error
 correction. (I find the latter much more engaging as a ham, since it
 is open source.) It would be a hoot to do a voice conference over the
 Internet using a sample of low bitrate codecs and just get a sense of
 what might be possible. One downside of voice is that it would occupy
 the transponder far more than messaging, and Bob's favorable power
 calculations would need to be estimated downwards.

 Would the packet satellite be capable of bent-pipe operation though?
 You'd need to transmit and receive simultaneously to get that working.
 I'd far prefer to use Speex rather than the locked-down proprietary AMBE
 codecs.

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[amsat-bb] Re: All Satellites (Alan P. Biddle)

2009-09-27 Thread John B. Stephensen
The 1200 bps Pacsats used an uncoded BPSK downlink on 70 cm and worked fine 
with 1/4-wavelength vertical antenna on the ground. As I remember, they only 
generated 1 watt of RF. A 2-meter downlink using an error correcting code 
would give 4 times the data rate with the same power. Digital voice now fits 
in 1200 bps so you could support APRS plus multiple voice channels.

73,

John
KD6OZH

- Original Message - 
From: Robert Bruninga bruni...@usna.edu
To: amsat-bb@amsat.org
Sent: Sunday, September 27, 2009 14:42 UTC
Subject: [amsat-bb] Re: All Satellites (Alan P. Biddle)


 And wouldn?t it be a hoot if [these cubesats]
 could put their RX/TX into a bent-pipe packet
 mode, and then we would have amateur radio
 global hand-held text messaging satellite system...

 Using some of the 2-way very small micro APRS
 packet systems, a 2 to 5 Watt transponder will
 easily fit... in a small cubesat.
 See  www.aprs.org/cubesat-comms.html

 If you could have maybe five or six cubesats
 with an FM transponder... [with] a good 15-minute pass
 every hour... would work wonders for getting people
 interested in satellites again.  ... [with a]
 dual-band HT and a homebrew Arrow clone

 The beauty of the APRS packet text-messaging relay cubesat is
 that it can have a 10 times higher power transmitter compared to
 an FM voice transponder for the same average power budget.  This
 makes it workable on an HT with just a whip antenna, instead of
 needing a handheld beam.  Plus, each message takes one second
 instead of 15 for each QSO.

 So that is why I prefer handheld packet text messaging as a
 cubesat mission.  Ten times the downlink power budget and 15
 times the number of contacts per pass.

 AO51 downlink could be 10 times as strong if the transmitter
 would just drop when not in use...

 Bob, WB4APR


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[amsat-bb] Re: Increasing range from LEO/SpaceX/APRS

2009-09-09 Thread John B. Stephensen
The sporadic thing about amateur satellites is free launch opportunuities. 
If hams were paying customers launches would be repeatable. Cubesats provide 
the standard form factor that fits many launchers and costs are less than 1% 
of a HEO launch.

73,

John
KD6OZH

- Original Message - 
From: Rocky Jones orbit...@hotmail.com
To: luclebla...@videotron.ca; Amsat BB amsat-bb@amsat.org
Cc: eu-am...@yahoogroups.com
Sent: Saturday, September 05, 2009 01:41 UTC
Subject: [amsat-bb] Re: Increasing range from LEO/SpaceX/APRS



 Luc...I would add this.

 What is firmly missing in the amateur satellite effort is something 
 repeatable that encourages solid commercial gear to be available to 
 people who want to use the sats.

 Wayne Green (w2nsd who I think is still with us)...had some pretty wild 
 stuff in the startup of the repeater movement...but he also had some 
 pretty good musings about what it would take to take the repeater movement 
 from the techies to ordinary hams...  He came and spoke to us while I 
 was in college and we had a chance to have some one on one and he more 
 or less nailed what it was going to take to get the repeater movement 
 mainstream.

 It is going to take about the same thing for hamsats...and one of those is 
 a continued supply of hamsats which encourage more communicating and less 
 experimenting

 Thats what is intriguing about the SpaceX launch campaign...and indeed 
 about the entire changes that are occurring now with the Augustine 
 commission there is a chance for things developing like geo synch rafts 
 where very large satellite complexes etc are built.  But ham radio will 
 not in my view have a seat at that table unless and until there is some 
 normalcy in the mode.

 I spent part of the afternoon talking with a condo owner on Clear Lake 
 about the Club moving its APRS/voice machine to the top of his 14 story 
 building (a virtual skyscraper in this part of Houston)...it was amazing 
 how fast he came around, all he could think of was what went on in 
 Hurricane Ike.

 Robert WB5MZO

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[amsat-bb] Re: Improving satellite reporting

2009-09-04 Thread John B. Stephensen
What are you using for reflow soldering?

73,

John
KD6OZH

- Original Message - 
From: William Leijenaar pe1...@yahoo.com
To: amsat-bb@amsat.org
Sent: Friday, September 04, 2009 13:29 UTC
Subject: [amsat-bb] Re: Improving satellite reporting


Hi AMSATs,

The tinny transponder design is finished and tested. I can make copies when 
there is interrest. My visit to Ham Fair in Tokyo was for me a kind of 
milestone to finish the design and make it public to the people. (I like to 
design something well done, before make it available to others, this avoids 
modifications and extra work later).

It is not easy to make the LE005-R2 transponder design without having the 
right tools. This is also the reason why I cannot sell it like a kit for 
people to solder at home.
The design is made at a profesional level (as development engineer I am 
dealing with it dayly) and can be made with use of a pick and place machine 
and reflow soldered for large quantities in a factory when needed. This is 
only profitable at large quantities.

For small quantities its cheaper and faster to do it with my small reflow 
system. The quality is guarenteed as I can do manual inspection and full 
testing myself.

The next step is doing space environment tests, but that takes some more 
time and money. In case you have a working thermal vaccuum chamber in your 
garage, let me know ;o)

The LE005-R2 is designed for space environment but not officially tested 
yet.
However, the design is well suited for applications like terresterial 
transponders.

73, with kind regards,
William Leijenaar, PE1RAH
---

- Original Message - 
From: Bruce Robertson ve9...@gmail.com
To: AMSAT-BB amsat-bb@amsat.org
Sent: Thursday, September 03, 2009 8:04 AM
Subject: [amsat-bb] Improving satellite reporting


[snip]


 (Similarly, I hope that William's extraordinary vision in building his
 transponder board might, after broad testing and examination, be
 validated by it becoming an 'AMSAT' off-the-shelf product. With
 William's approval, let's appeal for the bucks to have a team of
 people replicate these, test them, and set them up as temporary
 terrestrial repeaters around the world. We'd much more easily convince
 a cubesat team to include one of these if we could say one was running
 uninterrupted in Toronto for a year, or if we could have them do a QSO
 through one in a live demo!)


 73, Bruce
 VE9QRP


Hey, if William will make the boards available, I'll start building one
tomorrow!!!

73,

George, KA3HSW





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[amsat-bb] Re: Trolls on the -bb

2009-09-03 Thread John B. Stephensen
P3E is a HEO with the same engine as P3D and no benefactor funding a launch. 
It seems more reasonable to focus on projects that we can pay to launch or 
where someone has already donated the launch.

73,

John
KD6OZH

- Original Message - 
From: Luc Leblanc luclebla...@videotron.ca
To: amsat-bb@amsat.org
Sent: Wednesday, September 02, 2009 02:42 UTC
Subject: [amsat-bb] Re: Trolls on the -bb
 I know AMSAT has had it's issues over it's long history, and we are all
 disappointed that HEOs seem to be almost out of reach for us now. We are 
 all
 human and we all make mistakes, especially when it involves rocket 
 engines,
 building spacecraft on hobby store budgets, and getting all past our
 benefactor launch agency trials and schedules.

 If HEOs seem to be almost out of reach for us now what we should do 
 next? no more false illusions about geo sat's and so on just get back
 on earth and focused on how to help P3E and our German friend.

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[amsat-bb] Re: Trolls on the -bb

2009-09-03 Thread John B. Stephensen
Projects that we can afford means LEOs. P3A through P3D were built for 
identified launches. AMSAT shouldn't just sit around waiting for the right 
political climate for P3E.

73,

John
KD6OZH

- Original Message - 
From: i8cvs domenico.i8...@tin.it
To: John B. Stephensen kd6...@comcast.net; Luc Leblanc 
luclebla...@videotron.ca; AMSAT-BB amsat-bb@amsat.org
Sent: Thursday, September 03, 2009 09:51 UTC
Subject: [amsat-bb] Re: Trolls on the -bb


 It seems more reasonable to focus on projects that we can pay to launch

 All joined AMSAT togheter in the world has not the financial capability to
 pay for a HEO launch and this matter has been already discussed several
 time on this BB

 or  where someone has already donated the launch.

 Nobody has donated a launch for free or about for free on HEO except ESA 
 for
 OSCAR-10 OSCAR-13 and AO40 upon political strategy conducted mostly by
 AMSAT-DL and this is why we must pull for P3E...I agree completely 
 with
 Luc, VE2DWE

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[amsat-bb] Re: Trolls on the -bb

2009-09-03 Thread John B. Stephensen
Everyone also needs to understand that SDX makes more efficient use of 
limited downlink RF power. Less power means fewer extremely costly rad-hard 
solar panels and lower mass for reduced launch costs.

73,

John
KD6OZH

- Original Message - 
From: Bruce Robertson ve9...@gmail.com
To: John B. Stephensen kd6...@comcast.net
Cc: i8cvs domenico.i8...@tin.it; Luc Leblanc 
luclebla...@videotron.ca; AMSAT-BB amsat-bb@amsat.org
Sent: Thursday, September 03, 2009 17:50 UTC
Subject: Re: [amsat-bb] Re: Trolls on the -bb


On Thu, Sep 3, 2009 at 2:04 PM, John B. Stephensenkd6...@comcast.net 
wrote:
 Projects that we can afford means LEOs. P3A through P3D were built for
 identified launches. AMSAT shouldn't just sit around waiting for the right
 political climate for P3E.

 73,

I think that despite the difficulties in communication and personality
clashes, there is a great deal of agreement on the list about what we
want as a group.

We all want a HEO amateur communication satellite in orbit, some of us
because we've never had that experience, others because it is our
fondest memory of AMSAT operations. Barring that, or perhaps in
addition to that, we want to ensure that there are long-range
linear-transponder birds available in the future. Oddly enough,
despite all the rancor in recent days, none of it seems to be around
this core purpose of our group.

Some of our members seem to be concerned that because AMSAT is not
pursing this in a wholly direct way or because it is undertaking
projects of increased technical difficulty, it is therefore delaying
the fulfillment of the above primary goal.

It is my impression that the board members do not share this view.
They feel that the current impediment to a HEO launch in full-price
launch costs is so great that, for instance, the thousands spent on
SuitSat2 would never make a difference, since it is less than a
thousandth of the full price. Instead, we should make the best of
opportunities in LEO that might support our future work in HEO, MEO,
or wherever.

SuitSat2, since it will be the inaugural flight of the long-planned
SDX, is seen as fitting the strategy well. SDX is part of P3E and
proof that we are technically adept. This proof will be handy for
AMSAT-DL as it pursues the clearest path to the launch of P3E, namely
through government money that anticipates the mission to Mars.
According to this argument, pulling for P3E is no longer a matter of
saving pennies, but rather a matter of strutting our stuff, and SS2 is
a great way to strut and strut quickly. In this climate, enthusiasm
for SDX, SSE and, ultimately, P5 might be worth 100x any amount in
cash that we could give individually or as an organization.

Finally, SS2 provides a way of testing a core technology that might
become part of a module of a future bird, one built rapidly around a
launch opportunity.

I have to say that this strategy for fulfilling our common wishes
makes good sense to me.  It is predicated on some facts which I accept
at second hand: the high cost of HEO; the lack of government sponsored
launches in NA. I'm sure that the board would be delighted to have
their dismal assessment of *that* situation refuted conclusively. If
it cannot, then we must accept that sometimes the fastest route is not
the straightest path, but if we feel that this board is not guiding us
well towards our goals, we have the opportunity to replace our
pathfinders.

73, Bruce
VE9QRP

 John
 KD6OZH

 - Original Message -
 From: i8cvs domenico.i8...@tin.it
 To: John B. Stephensen kd6...@comcast.net; Luc Leblanc
 luclebla...@videotron.ca; AMSAT-BB amsat-bb@amsat.org
 Sent: Thursday, September 03, 2009 09:51 UTC
 Subject: [amsat-bb] Re: Trolls on the -bb


 It seems more reasonable to focus on projects that we can pay to launch

 All joined AMSAT togheter in the world has not the financial capability 
 to
 pay for a HEO launch and this matter has been already discussed several
 time on this BB

 or where someone has already donated the launch.

 Nobody has donated a launch for free or about for free on HEO except ESA
 for
 OSCAR-10 OSCAR-13 and AO40 upon political strategy conducted mostly by
 AMSAT-DL and this is why we must pull for P3E...I agree completely
 with
 Luc, VE2DWE

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[amsat-bb] Re: Increasing range from LEO.

2009-09-03 Thread John B. Stephensen
To get good coverage you need as many LEO satellites as possible so they should 
each be as small as possible. Intersatellite linking could be done via 
automated ground stations. This eliminates the need for high-power transmtters 
and/or high-gain antennas on the satellites for interlinkng. It's better to put 
that gain and power consumption on earth. Eveything on the satellite costs more 
than its weight in gold as launch costs are $700 per ounce.

73,

John
KD6OZH 
  - Original Message - 
  From: g0...@aol.com 
  To: kd6...@comcast.net ; amsat-bb@AMSAT.Org 
  Sent: Thursday, September 03, 2009 18:16 UTC
  Subject: Increasing range from LEO.


  In a message dated 03/09/2009 08:09:09 GMT Standard Time, kd6...@comcast.net 
writes:
P3E is a HEO with the same engine as P3D and no benefactor funding a 
launch. 
It seems more reasonable to focus on projects that we can pay to launch or 
where someone has already donated the launch.

73,

John
KD6OZH
  Wacky idea No 357

  Perhaps a longer term piece of AMSAT research could be to develop a subsystem 
for LEO satellites that detects and then connects users between passing LEOs. 
This would allow short term intersatellite communication.  Very tricky, but a 
nice project where boards are made available to anyone who would like to add 
this facility to their LEO Sat.

  Thanks

  David



 
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[amsat-bb] Re: Don't Fly SuitSat2 to ISS (rebuttal)

2009-08-23 Thread John B. Stephensen
The engine used in AO-40 was the same model used in all previous P3 series 
satellites.

AO-40's size was determined by the space donated by the ESA.

If the AMSAT-DL Mars mission is a fantasy then P3 may never fly as its 
launch is to be funded by that mission.

Suitsat seems perfectly reasonable as it is a UV linear transponder with the 
government paying for the launch. This is what most AMSAT members want.

73,

John
KD6OZH

- Original Message - 
From: Rocky Jones orbit...@hotmail.com
To: k...@sdf.lonestar.org; Amsat BB amsat-bb@amsat.org
Sent: Sunday, August 23, 2009 19:30 UTC
Subject: [amsat-bb] Re: Don't Fly SuitSat2 to ISS (rebuttal)



 Jeff...



 Clearly the kind of mistake that caused the catastrophic failure could
 have happened on any spacecraft assembled by any organization.

 nope.

 OK anyone has a statistical chance of dying or any project has a 
 statistical chance of failing but the more complex a project is the more 
 likely it is to fail...and AO-40 as it grew more complex needed larger 
 size which then needed a more powerful rocket engine...which ...

 this is mission creep (or more correctly design creep) and as I noted it 
 is a common cause of failure among homebuilders.  Unless you are rolling 
 your own (ie doing the aerodynamics yourself) most home builders build 
 something that professionals have at least deigned.  Where they get into 
 trouble is when they start adding things and making the project outside 
 the scope of what was well understood.

 had AO-40 not been supersat it would not have needed the larger 
 engine...


 You can call it simple if you like but a) it remains firmly affixed to
 earth and b) it is being sold to the German government as an adjunct to
 a mission to Mars. If you want to call an interplanetary mission
 simple that's your call, but P3E was scheduled to be launched years
 ago to support the P5 mission that was supposed to launch in 2009 and
 I'll buy the first beer whenever either of those fly...

 The one to Mars will never fly.Its a fantasy project..but 3E eventually 
 will.  I think.



 For the last time (from me, I promise) we have been told in no uncertain
 terms that the cost for a launch to GTO that would carry a craft of the
 size required to provide a happy medium of solar panels and antennas
 will cost no less than $6 million US and maybe as much as $8 million.

 If that is the case then we are, after 3E gets its launch done in HEO 
 sats...a reasonable hope is that with some new launch vehicles coming on 
 IE Falcon9 etc there might be some opportunities for reduced rate 
 launches...but who knows.  What I wonder is if there is any reluctance on 
 the part of launch vehicle providers after the 40 incident to let amateur 
 propulsion ride on their vehicle.  It is after all rocket science.

 Look my only argument is that reality should guide where the dollars are 
 spent, since as you point out, the dollars are not going as far as they 
 use to.  I bet suitsat is going to run (after all cost are figured in) 
 around 50,000 or so.

 thanks for a pleasant discussion...can pick this up later tonight but am 
 off for a little Mission creep myself.  Got the 51 foot tower up on the 
 new place at Santa Fe, but the XYL bought the tower of my dreams and we 
 are going to get it on its concrete stand today.

 later

 Robert WB5MZO



 _
 Get back to school stuff for them and cashback for you.
 http://www.bing.com/cashback?form=MSHYCBpubl=WLHMTAGcrea=TEXT_MSHYCB_BackToSchool_Cashback_BTSCashback_1x1
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[amsat-bb] Re: Lets Fix ISS, Replace ARISS

2009-08-17 Thread John B. Stephensen
P3E is part of the AMSAT-DL Mars mission and the launch depends on German 
government funding rather than amateur funding. Why not make use of a nearly 
free launch opportunuty as AMSAT-NA is doing?

73,

John
KD6OZH

- Original Message - 
From: Rocky Jones orbit...@hotmail.com
To: ka1...@yahoo.com; Amsat BB amsat-bb@amsat.org
Sent: Sunday, August 16, 2009 20:57 UTC
Subject: [amsat-bb] Re: Lets Fix ISS, Replace ARISS



Miles..What I dont get, but to be fair to AMSAT I have not had a lot of time 
to pay attention to...is why some projects are going on and why some of 
those are going where they are going.

Suitsat for instance.

It started out as a pretty simple effort to make use of discarded equipment. 
OK the first one had some problems but those could have been troubleshooted 
and fixed and then something similar be readied for the next opportunity 
to fly.

Now if one reads what is up on line and in AMSAT the project has morphed 
quite a bit...and worse as best as I can tell looking at the station 
manifest, the Russian suits are gone.  IE the used ones were tossed into the 
progress around July and dumped into the Pacific...there is still some 
uplift possibility and apparently a deployment in 2010...but as best I can 
see what they are going to have to put together is an actual frame of some 
sort which along with the payload has bumped up the complexity a bit.

If they get into trying to get the strows on board to try and actually 
doing a lot of assembly that will I bet flounder in short order.

So with money needed for the launch cost for P3E...why is this project going 
on?  At best it is a very short term flight.

For all I know this has been discussed on line, I am moving into a new 
airplane and when that starts happening I sort of drop out of the world for 
the months that takes...but...

ISS is going to change.  If you have been following the Augustine commission 
there is likely to be some massive changes in how ISS is accessed over the 
next 5-10 years...Amsat probably is but in any event should be moving to 
make some inroads in that access.

there is also likely to be some massive changes in how ISS is operated (but 
that is another story).

Robert WB5MZO Amsat life member



 From: orbit...@hotmail.com
 To: ka1...@yahoo.com; amsat-bb@amsat.org
 Date: Sat, 15 Aug 2009 12:37:40 -0500
 Subject: [amsat-bb] Re: Lets Fix ISS, Replace ARISS


 Miles.  well done.  I suspect that you have hit a brick wall...but I 
 concur in everything you wrote.

 Having said that.  ISS and human spaceflight in general (at least in the 
 US) is on the verge of a very big shake up...and that might shake the ham 
 equation as well.

 Robert Oler WB5MZO

  Date: Sat, 15 Aug 2009 10:20:38 -0700
  From: ka1...@yahoo.com
  To: amsat-bb@amsat.org
  Subject: [amsat-bb]  Lets Fix ISS, Replace ARISS
 
  Marex
 
  Miles Mann WF1F
 
  Marex
 
  w...@marexmg.org
 
 
 
  August 25, 2009
 
  Dear ARISS supporters:
 
  I am writing to you because of the extremely poor track record that 
  ARISS has accumulated over the past 12 years regarding ISS hardware 
  projects.
 
  The only way to correct the problem and fix the Amateur Radio 
  educational program is to completely reorganization the current ARISS 
  hardware structure.
 
  Under the new ARISS Closed Door policy, only selected members from 
  AMSAT-NA are allowed to participate.
 
  This new policy has turned the once open ARISS into a closed door 
  Monopoly controlled by the AMSAT Corporation.
 
  Based on the current actions of ARISS and their very poor performance 
  with in-flight hardware I would like to propose a complete 
  reorganization of the ARISS hardware process.
 
  Please review the enclosed information.
 
  I look forward to discussing the proposal with you are your earliest 
  opportunity.
 
  Sincerely
 
  G. Miles Mann
 
 
 
 
 
  Memo from ARISS April 2009
 
  From Gaston Bertels ARISS Chairman
 
  Hi Miles,
 
  By decision of the ARISS Board, participation to ARISS-i meetings is 
  limited to delegates from the Member Societies and observers nominated 
  by these societies.
 
  USA member societies are the ARRL and AMSAT NA.
 
  Only these societies can nominate participants to the ARISS-i meetings.
 
  Best regards
 
  73
 
  Gaston Bertels, ON4WF
 
  ARISS Chairman
 
 
 
 
 
 
 
 
 
 
 
  ARISS Reorganization Proposal
 
  By Miles Mann
 
  June 17, 2009
 
  Rev 1.01
 
 
 
  What is ARISS?
 
  The goal of ARISS was to create an organization to select, control and 
  coordinate Amateur Radio projects designed for the International Space 
  Station (ISS).
 
  The ARISS program would then assist the 16 countries (Russia, Canada, 
  Japan, Brazil, USA, member nations of ESA, Belgium, Denmark, France, 
  Germany, Italy, The Netherlands, Norway, Spain, Sweden, Switzerland, and 
  the United Kingdom), which are supporting the ISS to help choose the 
  best educational Amateur Radio projects for ISS.
 
  Each county would have delegate-voting 

[amsat-bb] Re: Your Own Personal Satellite

2009-08-03 Thread John B. Stephensen
However, the IC-7800 doesn't stop working after 3 weeks.

73,

John
KD6OZH

- Original Message - 
From: Jeff Davis jeffrey.da...@mac.com
To: AMSAT BB amsat-bb@amsat.org
Sent: Sunday, August 02, 2009 14:19 UTC
Subject: [amsat-bb] Your Own Personal Satellite


For MUCH less than the price of an IC-7800...

Planet Earth has entered the age of the Personal Satellite with the
introduction of Interorbital’s TubeSat Personal Satellite (PS) Kit.
The new IOS TubeSat PS Kit is the low-cost alternative to the CubeSat.
It has three-quarters of the mass (0.75-kg) and volume of a CubeSat,
but still offers plenty of room for most experiments or functions.

And, best of all, the price of the TubeSat kit actually includes the
price of a launch into Low-Earth-Orbit on an IOS NEPTUNE 30 launch
vehicle. Since the TubeSats are placed into self-decaying orbits 310
kilometers (192 miles) above the Earth’s surface, they do not
contribute to any long-term build-up of orbital debris. After a few
weeks of operation, they will safely re-enter the atmosphere and burn-
up. TubeSats are designed to be orbit-friendly.  Launches are expected
to begin in the fourth quarter of 2010.
Total Price of the TubeSat Kit including a Launch to Orbit is $8,000!

http://spacefellowship.com/2009/08/01/interorbital-syatems-tubesat-personal-satellite-kit/
 

--
Jeff, KE9V
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[amsat-bb] Re: Your Own Personal Satellite

2009-08-03 Thread John B. Stephensen
The space and mass required for the fuel and attitude control system would be 
prohibitve. CubeSats are better solution for a communications satellite as you 
get 10 years of 20 minute passes rather than 3 weeks of 10 minute passes. A 3U 
CubeSat might barely have enough space for an engine, attitude control and fuel 
but you'd end up with something like Arsene (AO-24).

73,

John
KD6OZH
  - Original Message - 
  From: Joe 
  To: John B. Stephensen 
  Sent: Tuesday, August 04, 2009 04:01 UTC
  Subject: Re: [amsat-bb] Re: Your Own Personal Satellite


  hopw much energy is needed to bost it to a higher orbit?

  John B. Stephensen wrote:

However, the IC-7800 doesn't stop working after 3 weeks.

73,

John
KD6OZH

- Original Message - 
From: Jeff Davis jeffrey.da...@mac.com
To: AMSAT BB amsat-bb@amsat.org
Sent: Sunday, August 02, 2009 14:19 UTC
Subject: [amsat-bb] Your Own Personal Satellite


For MUCH less than the price of an IC-7800...

Planet Earth has entered the age of the Personal Satellite with the
introduction of Interorbital's TubeSat Personal Satellite (PS) Kit.
The new IOS TubeSat PS Kit is the low-cost alternative to the CubeSat.
It has three-quarters of the mass (0.75-kg) and volume of a CubeSat,
but still offers plenty of room for most experiments or functions.

And, best of all, the price of the TubeSat kit actually includes the
price of a launch into Low-Earth-Orbit on an IOS NEPTUNE 30 launch
vehicle. Since the TubeSats are placed into self-decaying orbits 310
kilometers (192 miles) above the Earth's surface, they do not
contribute to any long-term build-up of orbital debris. After a few
weeks of operation, they will safely re-enter the atmosphere and burn-
up. TubeSats are designed to be orbit-friendly.  Launches are expected
to begin in the fourth quarter of 2010.
Total Price of the TubeSat Kit including a Launch to Orbit is $8,000!

http://spacefellowship.com/2009/08/01/interorbital-syatems-tubesat-personal-satellite-kit/
 

--
Jeff, KE9V
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[amsat-bb] Re: FUNcube a UK Linear Transponder Satellite

2009-07-25 Thread John B. Stephensen
Yes, there are lots of launch opportunities for LEO satellites. They aren't 
free, but very inexpensive compared to a HEO satellite. You get a 800 km 
orbit (like AO-51) for a 10 x 10 x 10-30 cm payload. The standard size 
reduces overhead so you can afford to launch a very small satellite as one 
of a group of 6 or more for a little more than $10,000 per pound.

73,

John
KD6OZH

- Original Message - 
From: David - KG4ZLB kg4...@googlemail.com
To: amsat-bb@amsat.org
Sent: Saturday, July 25, 2009 18:59 UTC
Subject: [amsat-bb] Re: FUNcube a UK Linear Transponder Satellite


/**//*It is anticipated FUNcube will be launched into a Sun Synchronous
Low Earth Orbit about 600-700km above the earth using one of the many
launch opportunities that exist for Cubesat missions.*/

*_Many_* launch opportunities ???

-- 
David
KG4ZLB
www.kg4zlb.com





David Johnson wrote:
 Hi,

 AMSAT-UK has announced a new amateur satellite project – FUNcube – that
 features a 435 to 145 MHz Linear Transponder for SSB/CW operation. The
 project has received major initial funding from the Radio Communications
 Foundation (RCF) and is expected be developed in collaboration with
 ISIS-Innovative Solutions in Space BV.

 FUNcube is an educational single cubesat project with the goal of
 enthusing and educating young people about radio, space, physics and
 electronics.

 It will support the educational Science, Technology, Engineering, Maths
 (STEM) initiatives and provide an additional resource for the GB4FUN
 Mobile Communications Centre.

 The target audience consists of primary and secondary school pupils and
 FUNcube will feature a 145 MHz telemetry beacon that will provide a
 strong signal for the pupils to receive.

 It is planned to develop a simple receiver board that can be connected
 to the USB port of a laptop to display telemetry in an interesting way.

 The satellite will contain a materials science experiment, from which
 the school students can receive telemetry data which they can compare to
 the results they obtained from similar reference experiments in the
 classroom.

 FUNcube is the first cubesat designed to benefit this group and is
 expected to be the first UK cubesat to reach space.

 More details can be found at:

 http://www.uk.amsat.org/content/view/696/68/

 73
 Dave, G4DPZ
 AMSAT-UK 1267
 AMSAT-NA LM-1260
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-- 
David
KG4ZLB
www.kg4zlb.com

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[amsat-bb] Re: AMSAT Officer Assistance

2009-07-20 Thread John B. Stephensen
97.113 (5) (c) A control operator may accept compensation as an incident of 
a teaching position during periods of time when an amateur station is used 
by that teacher as part of classroom instruction at an educational 
insitution.

73,

John
KD6OZH

- Original Message - 
From: Timothy J. Salo s...@saloits.com
To: amsat-bb@amsat.org
Sent: Monday, July 20, 2009 17:42 UTC
Subject: [amsat-bb] Re: AMSAT Officer Assistance


 Related to Q2  Q5 (compensation):
 * As university staff, can I transmit to the CubeSat, or is my
 salary considered compensation?

 * Is the refurbishment of a club ground station (man hours,
 equipment repair/purchase) considered compensation?

 These are very important questions.  I think it is also
 important that we have a shared understanding of the answers,
 rather than private opinions.

 I suggest that the researcher also approach the ARRL for an
 opinion.  My suspicion is that AMSAT and the ARRL will provide
 conservative (and unofficial) answers to these questions.  It
 is much safer to say no, that's prohibited than yes.

 In my view, this may be a question that we want to approach
 the FCC with.  I suspect that, if the question is properly
 framed, the FCC might be more inclined to find this acceptable
 than either AMSAT or the ARRL.

 -tjs

 Clint Bradford wrote:
 Can an AMSAT officer please privately reply to me regarding this email
 inquiry? Many thanks.

 A gentleman is considering a CubeSat mission for weather research, and
 needs answers to his inquiry after reading the AMSAT FAQ regarding
 using ham frequencies ...


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[amsat-bb] Re: ILN... Is this our future ride to the moon? MM

2009-07-06 Thread John B. Stephensen
Hi Miles,

Since the rest of us on this BB don't have any details about the landers, it 
would be useful if you could get a copy of any RFP (request for proposal) 
and find out how much DC power will be available for how long, how much 
weight and surface area could be allocated for the package and what type of 
experiments NASA is interested in. Then we could calculate what could be 
provided for an RF downlink to earth and how many people could use it.

73,

John
KD6OZH

- Original Message - 
From: MM ka1...@yahoo.com
To: James French w8...@wideopenwest.com
Cc: amsat-bb@amsat.org; Armando Mercado am25...@triton.net
Sent: Monday, July 06, 2009 14:26 UTC
Subject: [amsat-bb] Re: ILN... Is this our future ride to the moon? MM





 The Amateur radio community does not have the resources to build a better 
 communication system than a professional commercial company.

 So we have two options, use existing lander hardware for communication or 
 design our own stand alone transceiver project that just uses existing 
 power and or antennas.

 After the lander has released the Rover, the lander “May” have some unused 
 resources.  Lets see if any of these unused resources (if any) can be used 
 for Amateur Radio projects.

 How is the Lander going to be powered?
 Batteries only:
 If so, there will be no power for projects.  The lander telemetry will 
 stop after a few days.  This is not a likely scenario.

 Solar Panels and Batteries:
 In this option, there may be some available power during lunar days to run 
 other projects.  This is the most sensible solution.

 Atomic Battery:
 This is the best option, however it’s politically sensitive.
 http://en.wikipedia.org/wiki/Atomic_battery

 The power source is one of the keys to designing a possible Amateur Radio 
 project.  Let’s ping our contacts at NASA and see what we can learn about 
 the Moon Lander projects.

 Flash Back:
 On ISS, the Russian team proposed that we re-use navigation antennas from 
 the FGB modules for Amateur Radio (1996).  The  idea worked and on the 
 very first ISS mission we had access to an already installed antenna.  It 
 was a simple idea and it worked.

 Education Spin:
 Contributing to the project from a scientific nature may be difficult, we 
 will have to get some universities involved, or we could focus on the 
 educational nature of the project.
 Lets try to put the educational spin that School and university are 
 communication via the Moon, with radio station designed and built by the 
 schools.

 I am not saying that NASA would approve this project, but until we try we 
 will not know.
 This project does not have to be an AMSAT project, we can make it a 
 University project.


 Sincerely Miles WF1F


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[amsat-bb] Re: dream your own sat

2009-07-05 Thread John B. Stephensen
The problem is that amateur radio doesn't significantly reduce the cost of a 
satellite. Any interest by the Red Cross would not be in the satellite but 
in human volunteers that might come with it. Unfortunately, the LEO 
satellites that hams can afford generate little interest in this forum.

73,

John
KD6OZH

- Original Message - 
From: Art McBride kc6...@cox.net
To: 'rupert red' rupert@live.it; amsat-bb@amsat.org
Sent: Sunday, July 05, 2009 19:00 UTC
Subject: [amsat-bb] Re: dream your own sat


 Rupert,
 I think that is a fair assumption on your part, but only because the are 
 no
 new ideas being presented that have commercial potential that can use
 Amateur Radio as an inexpensive to proof of concept.
 In the present Amateur Radio community only Emergency Communications is
 getting the publicity. Perhaps FEMA or the Red Cross might help pay for an
 emergency communication satellite otherwise it is LEO's forever!

 Art, KC6UQH

 -Original Message-
 From: amsat-bb-boun...@amsat.org [mailto:amsat-bb-boun...@amsat.org] On
 Behalf Of rupert red
 Sent: Sunday, July 05, 2009 4:47 AM
 To: amsat-bb@amsat.org
 Subject: [amsat-bb] dream your own sat


 Hallo all...

 from a while I'm hearing about MANY different and interesting satellite
 solutions...

 LEO, MEO, HEO, GEO... MOON !!!

 The problem is only ONE !

 Amateur radio community has no money for this project, and will never 
 have!

 Amsat  Co will never be able to collect millions I red on this bb 
 that
 hams has no money for an expensive ground station... then how can they 
 send
 many money to Amsat?

 Public and private organizations all over the world have not an high
 consideration of hams, and will never invest founds for them.

 The conclusion is only ONE... we will never see a new oscar satellite in 
 the
 sky (at least some student's cube).

 Let's all dream together guys.



 Best 73 Rupert

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[amsat-bb] Future satellites

2009-07-04 Thread John B. Stephensen
An interesting question for the short term is what can we do with 1 watt of 
RF from a LEO satellite. RS-10 and RS-12 were interesting as they required 
only omnidirectional antennas but they had a lot of power available as they 
were attached to much larger satellites. AO-16 was a small satellite but was 
capable of only 1200 bps data using uncoded BPSK and simple vertical 
antennas.

Given the type of hardware developed for Suitsat-2, we should be able to do 
a lot more. Using modern error-correcting codes 4800 bps is possible using 
omnidirectional antenas and with modern codecs that can carry 4 voice 
channels or 3 voice channels plus 40 PSK31-like channels. With 10 dBi of 
gain at the ground station the data rate and number of voice channels could 
be quadrupled. The downlink could also be split between 2 voice channels for 
use with omnidirectional antennas and 8 voice channels for high-gain 
antennas.

73,

John
KD6OZH

I have extracted from it the most important following part:

73 de

i8CVS Domenico

Extracted from G3RUH article THE EARTH MOVES

 An example, 1 watt transmitted from a 20 dbi gain dish on the Moon,
 received on a 1.2m dish at Earth with a system noise temperature of 100K
 results in a signal to noise ratio in 2.4 kHz bandwidth of 10.5 db. (Note
 that frequency matters not). This would support one rather noisy SSB voice
 signal.
 Alternatively it would carry an error-free 2400 bps binary PSK data
 transmission without coding, 9600 bps with modest coding [2].

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[amsat-bb] Re: The Moon is our Future

2009-07-03 Thread John B. Stephensen
Actually, its very bad as it barely supports 1 user at 3 times the proposed 
maximum power level. You could support 100 users on a HEO with the same SNR and 
power output. Most users will consider 10 dB SNR to be marginal and want 
another 10 dB of signal strength on the downlink. The same amount of power has 
been consumed by 10 stations on HEOs.

73,

John
KD6OZH 
  - Original Message - 
  From: Joe 
  To: John B. Stephensen ; amsat-bb@amsat.org 
  Sent: Thursday, July 02, 2009 22:01 UTC
  Subject: Re: [amsat-bb] Re: The Moon is our Future


  Now thats pretty good!

  But why is it soo good,  when  the HEO birds were soo hard?

  something missing?

  John B. Stephensen wrote:

Path loss for a lunar downlink at 435 MHz is 197 dB and the sky temperature 
is about 75 K. If you assume a 2.5 kHz wide SSB voice downlink and 10dB 
average SNR (16 dB peak) a perfect receiver needs to see -130 dBm PEP input. 
Given 5 dBic of gain on the moon and 17 dBic (one long yagi) of gain on the 
earth, the lunar transmitter needs to provide +45 dBm PEP (32 Watts) per 
user.

73,

John
KD6OZH

- Original Message - 
From: MM ka1...@yahoo.com
To: kg4...@gmail.com; amsat-bb@amsat.org; Jack K. kd1p...@gmail.com
Sent: Thursday, July 02, 2009 11:31 UTC
Subject: [amsat-bb] The Moon is our Future


  Theoretically we may have a free ride to the Moon for an Amateur radio 
repeater!

In the past, the flight to the moon for a Amateur radio project has been 
cost prohibitive.  We just could not afford to pay for the ride to the 
Moon.
NASA is going to the moon with unmanned landers. NASA is open to the idea 
of flying some public service projects to the moon on their landers.

Now there exists the possibility of getting a free ride to the moon, 
curtsy of NASA.

What we need are the following:

A stable club with funding to build a simple transponder project.
A plan for a simple transponder (KISS  no complex P3E).
A link budget plan for a Moon transponder.


One theory:
We need a simple Mode-J transponder (2-meters up, 440 down).
Low power consumption.
Assume minimal antenna gain from the Lander (3 dBd on each antenna)
Assume transmitter power 5-10 watts.

Questions:
What’s the link budget?
How much gain will be needed on earth for such a setup?
Can we build a working mockup in 1 year or less.

The Moon is within Reach.  Let’s Go for IT.

Miles WF1F   MarexMG.org


--- On Wed, 7/1/09, Jack K. kd1p...@gmail.com wrote:

From: Jack K. kd1p...@gmail.com
Subject: [amsat-bb]  Rebuttal -  Re: Unused sats
To: kg4...@gmail.com, amsat-bb@amsat.org
Date: Wednesday, July 1, 2009, 4:46 PM
I have to disagree in the strongest
of terms about disregarding HEOs for
now which in essence will mean to become forever. Until,
or unless, we
could come up with something along the lines of a Cell
system of leos, we
are missing one of the major advantages of Satellites and
that is almost
guaranteed communications for long periods (several hours)
at a time... I am
in no way denigrating LEOs as they have their place, but in
the major schema
of things HEOS will and always have rule given the state of
communications
art...

I understand the desire to do something but I suggest
that the major
thrust should be directed at getting a transponder on the
moon (or Mars) or
some more KISS type HEOs up... Cubesats can take care of
themselves if we
do, Heck I would even join in and participate in something
like I just
mentioned, I just can not get excited about Contest style
contacts with a
5-12 min window most of the time... I do that on 2 meters
scatter all I
want,

DE Jack - KD1PE


- Original Message - 
From: David - KG4ZLB kg4...@googlemail.com
To: amsat-bb@amsat.org
Sent: Wednesday, July 01, 2009 4:09 PM
Subject: [amsat-bb] Re: Unused sats


  All good points but forget the HEO's for now - we just
need a good
  source of regularly launched easy sats in LEO to
augment the few working
  birds we have and replace what we have to as they fall
out of the sky or
  just stop working.
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[amsat-bb] Re: The Moon is our Future

2009-07-03 Thread John B. Stephensen
A more meaningful appoach for an exercise like this is to start with DC 
power input for the entire package. Receivers consume power and transmitters 
(especially linear ones) are inefficient and the efficency goes down with 
increasing frequency. On the moon, you also have to heat the electronics at 
night to prevent failure.

Linear microwave power amplifiers have 20-35% efficiencies and VHF 
amplifiers might reach 50%. You can make more efficient amplifiers by 
converting the output signal into magnitude and phase or frequency 
components and using class C, D or E amplifiers. However, the added 
circuitry (whether analog or digital) also consumes power. FM makes sense 
for single channel transponers as the amplifiers can be nonlinear and you 
can get 80% efficiency at VHF. SSB amplifiers have a double inefficiency as 
you must design for peak power output which is 4-5 times the average power 
output. Amateur HEO satellites have used SSB for multichannel applications 
as you can count on the voice peaks for different users to occur at 
different times and design for the average power of all users. However, you 
need lots of users to reach this goal.

73,

John
KD6OZH

- Original Message - 
From: i8cvs domenico.i8...@tin.it
To: Joe n...@mwt.net
Cc: Jack K. kd1p...@gmail.com; AMSAT-BB amsat-bb@amsat.org; 
kg4...@gmail.com
Sent: Friday, July 03, 2009 14:41 UTC
Subject: [amsat-bb] Re: The Moon is our Future


 Hi Joe,

 The specification given by Miles WF1F is for a Lander transmit power of 5 
 to 10 watt in 70 cm from the moon.My calculation shoves that a single SSB 
 station to be received in 70 cm with a S/N ratio of 10 dB on the earth a 
 power of 10 watt in 70 cm is necessary on the moon.

 If you like an IF window 10 time greater i.e. 250 KHz to accomodate more 
 stations at the same time than the Lander transponder must have the 
 capability to get around 100 watt wich is out the WF1F specifications.

 73 de

 i8CVS Domenico
  - Original Message - 
  From: Joe
  To: i8cvs
  Cc: MM ; kg4...@gmail.com ; AMSAT-BB ; Jack K.
  Sent: Friday, July 03, 2009 12:59 PM
  Subject: Re: [amsat-bb] Re: The Moon is our Future


  This is all good except for one thing,

  The IF window is 10 times too small.

  Look at the mess the FM single channel birds are with their tiny surface 
 foot print.  Imagine now a whole hemisphere worth of people trying to use 
 it at once.  The thing would be useless

  i8cvs wrote:
 - Original Message -
 From: MM ka1...@yahoo.com
 To: kg4...@gmail.com; amsat-bb@amsat.org; Jack K. 
 kd1p...@gmail.com
 Sent: Thursday, July 02, 2009 1:31 PM
 Subject: [amsat-bb] The Moon is our Future


 We need a simple Mode-J transponder (2-meters up, 440 down).
 Low power consumption.
 Assume minimal antenna gain from the Lander (3 dBd on each antenna)
 Assume transmitter power 5-10 watts.

 Questions:
 What’s the link budget?
 How much gain will be needed on earth for such a setup?
 Can we build a working mockup in 1 year or less.

 The Moon is within Reach.  Let’s Go for IT.

 Miles WF1F   MarexMG.org


 Hi Miles, WF1F

 The gain of the 2 meters antenna on the Lander is 3 dBd = 5.14 dBi
 Assume that the Noise Figure of the 2 meter receiver is 0.5 dB = 35 kelvin
 and the sky temperature as seen by the 2 meter Lander antenna looking at
 the earth is conservatively 290 kelvin but (probably more ).
 The isotropic path loss earth-moon in 2 meters at an average distance of
 380.000 km is 187 dB
 You don't specify the IF bandwidth of your transponder so that for
 simplicity I will assume that only one QSO will be possible in SSB and 3
 on CW in a total BW = 2.5 KHz
 With the above data the calculated Noise Floor (KTB) of the above 2 meter
 Lander receiver is  -139 dBm
 We assume to use an earth 2 meters antenna with a gain of 13 dBi and a 
 power
 of 100 watt pep in 2 meters.

 UPLINK BUDGED:

 Earth TX  power  100 watt.+ 50 dBm
 Earth antenna gain. .+ 13 dB
  --
 Earth EIRP.+ 63 dBm
 2 m  isotropic attenuation earth-moon..-187 dB
  --
 Isoptropic power received on the moon .- 124 dBm
 2 meters Lander antenna gain.+ 5 dBi
  --
 Power applied to the 2 m Lander receiver..- 119 dBm
 Lander receiver 2 m Noise Floor...-  139 dBm
  --
 S/N ratio available from the Lander receiver.. +  20 dB

 COMMENT:
 With a 2 meter signal +20 dB above the noise floor the
 70 cm TX on the Lander transponder is in condition to
 supply a noise-less power between 5 to 10 watt pep to
 the 70 cm TX antenna.

 DOWNLINK BUDGED:

 The gain of the 

[amsat-bb] Re: The Moon is our Future

2009-07-03 Thread John B. Stephensen
HEOs are illuminated 99% of the time and LEOs are illuminated 50% or more of 
the time with eclipses by the earth lasting only 45 minutes. Thermal inertia 
can keep the temperature from swinging too far in either direction. Since the 
satellite is in a vacuum, heat can only be radiated away as in a Dewar flask. 
On the moon, the eclipse lasts for 2 weeks so more cooling occurs. During the 
other 2 weeks, heat from the electronics and solar illumination must be 
radiated away. Every lander that I have seen has a few spindly legs so there 
won't be much heat conduction to the moon's surface.

However, I'm not an expert on thermal design. When I was designing a 70 cm 
receiver for AMSAT, others did the thermal analysis. Nothing behaves in space 
as it does on Earth as there is no convection cooling. 

Building a prototype that works on Earth for project like this is only a few 
percent of the effort required. Treating it as a radio club project won't be 
effective as people need to sign up for a 5-year project. If your making an 
add-on to a NASA project you have to fit into their shedule, design to their 
specifications, produce the documentation that they need, travel to their test 
facilities and pass their tests. There are also legal requirements (ITAR) when 
working on space-related projects.

73,

John
KD6OZH
  - Original Message - 
  From: Joe 
  To: John B. Stephensen 
  Cc: i8cvs ; Jack K. ; AMSAT-BB ; kg4...@gmail.com 
  Sent: Friday, July 03, 2009 19:57 UTC
  Subject: Re: [amsat-bb] Re: The Moon is our Future


  Been Thinkin',

  John B. Stephensen wrote:

A more meaningful appoach for an exercise like this is to start with DC 
power input for the entire package. Receivers consume power and transmitters 
(especially linear ones) are inefficient and the efficency goes down with 
increasing frequency. On the moon, you also have to heat the electronics at 
night to prevent failure.
  What difference is there and why if there is any a difference of  shadow cold 
on the moon,  vs  shadow in orbit?  If anything i would think you would get 
some thermal radiation heating from the soil.  wjereas in space you don't get 
this benefit.

  
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[amsat-bb] Re: NASA Kills Ulysses

2009-07-01 Thread John B. Stephensen
This sounds like the AMSAT-Intelsat deal except that the Intelsat agreement 
would allow the amateur payload to operate in parallel with the primary 
payload. A number of the RS series amateur satellites also operated this 
way.

73,

John
KD6OZH

- Original Message - 
From: STeve Andre' and...@msu.edu
To: amsat-bb@amsat.org
Sent: Wednesday, July 01, 2009 16:49 UTC
Subject: [amsat-bb] Re: NASA Kills Ulysses


 Thats a neat idea.  We'd have to build the whatever to the physical
 specs provided, and pay for the extra fuel needed.  Sadly, I think
 in order to make this work we're talking real money, but perhaps I
 am wrong.  Perhaps there is a tax-writeoff somehow?  I'd like to
 hear of what the amsat folks have thought of along these lines;
 they know of the conditions of business in the field.

 --STeve Andre'
 wb8wsf  wn82

 On Wednesday 01 July 2009 12:43:39 David - KG4ZLB wrote:
 I know it would be expensive but on the if you spread your net wide
 enough view of thinking, could we not approach commercial satellite
 projects prior to launch and bung a transponder on them only to be used
 when the primary mission fails? OK, so you might win some, might lose
 some and I know it would be expensive but it seems better than the
 situation we have now, plus we could be potentially building in some
 long term birds that would replace the current ageing fleet. It would be
 a long term view, but it would be something!

 Presumably this has been brought up before but no harm in re-hashing it
 for any new ideas especially with the BoD voting soon to happen! :-D

 73

 David

 -
 David
 KG4ZLB
 www.kg4zlb.com

 STeve Andre' wrote:
  About the only thing we could do is use them as training guides for
  receiving weak signals.  Satellities are not designed to qsy, or do
  anything other than they actual function(s), specified long before
  they were ever built.  Add more to a bird increases complexity, and
  also failures.
 
  I'll bet they turned it off to free up that frequency for something
  else.  If that is the case then we can't even really try monitoring.
 
  I've often wondered about the ham community using old systems
  but except for really rare cases, they are just too specific to do
  anything for us.
 
  --STeve Andre'
  wb8wsf  en82
 
  On Wednesday 01 July 2009 12:13:19 w7...@comcast.net wrote:
 
 
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[amsat-bb] Re: Gold plated contact

2009-06-13 Thread John B. Stephensen
63/37 solder works fine but it wicks up the contact very quickly.

73,

John
KD6OZH

- Original Message - 
From: Luc Leblanc luclebla...@videotron.ca
To: amsat-bb@amsat.org
Sent: Saturday, June 13, 2009 19:28 UTC
Subject: [amsat-bb] Gold plated contact


 Did any one has ever try to solder on gold metal contact pin? Is the 
 standard electronic solder is ok or?


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 Luc Leblanc VE2DWE
 Skype VE2DWE
 www.qsl.net/ve2dwe
 WAC BASIC CW PHONE SATELLITE



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[amsat-bb] Re: Satellite funding sources!

2009-05-06 Thread John B. Stephensen
Note that these are opportunties are for LEO satellites like AO-51.

73,

John
KD6OZH

- Original Message - 
From: Luc Leblanc luclebla...@videotron.ca
To: amsat-bb@amsat.org
Cc: eu-am...@yahoogroups.com
Sent: Tuesday, May 05, 2009 13:21 UTC
Subject: [amsat-bb] Satellite funding sources!



 It seems that money is available and it is advertised publicly! I don't 
 know if AMSAT-NA is aware of it? interested in it? sensible to it?
 able to refocused quickly their goals if any remains? Is a joint support 
 offer to some researchers can be something to be explore?

 But in the mean time amateur are bystanders spinning their wheels on 
 ice...

 Here is the text:

 Please be advised that the NSF Proposal  Award Policies  Procedures 
 Guide (PAPPG) includes revised guidelines to implement the mentoring
 provisions of the America COMPETES Act (ACA) (Pub. L. No. 110-69, Aug. 9, 
 2007.) As specified in the ACA, each proposal that requests
 funding to support postdoctoral researchers must include a description of 
 the mentoring activities that will be provided for such
 individuals. Proposals that do not comply with this requirement will be 
 returned without review (see the PAPP Guide Part I: Grant Proposal
 Guide Chapter II for further information about the implementation of this 
 new requirement).

 Beginning in 2009, NSF expects to launch two to three P-PODs every year, 
 accommodating at least as many (two to six) individual satellite
 missions.  This solicitation covers proposals for science missions to 
 include satellite development, construction, testing and operation as
 well as data distribution and scientific analysis.

 More details at 
 :http://www.nsf.gov/publications/pub_summ.jsp?ods_key=nsf09523


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 Luc Leblanc VE2DWE
 Skype VE2DWE
 www.qsl.net/ve2dwe
 WAC BASIC CW PHONE SATELLITE



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