[amsat-bb] NASA - 2011/2012 CubeSat Launch Opportunities

2010-02-27 Thread Trevor .
See 

http://prod.nais.nasa.gov/cgi-bin/eps/synopsis.cgi?acqid=139845 
 
73 Trevor M5AKA



  


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[amsat-bb] Re: Planet Pseudo-Keps

2010-02-27 Thread Jeff Yanko
Hi Bob,

You are correct on the term planets being wonderers.  If I recall 
correctly, that came from the Greek skywatchers.

Yes, many thought the Earth was the center of the solar system.  I'm sure 
more believed it was the center of the universe as well!  In any case, with 
the Sun as the center of the solar system, that was some wild outside of 
the box thinking since the church frowned upon any type of new findings 
that disputed what the church layed down.  Can you imagine being ostracized, 
if nothing more serious, in stating and believing that the Sun, not the 
Earth, was the center of the solar system?  WOW!  You'd be excommunicated 
and strung up.

Since the planets revolve around the Sun ,and not the Earth, there can't be 
any Keps.  Keps are based on the Earth being the center of an orbiting 
object.  I should've recalled that.  However, my thinking at the time was if 
there are programs which display where to find planets in the sky, like 
Starry Night, then there'd have to be a form of calculation to determine it. 
I just thought of using the wrong type of calculation.


73,

Jeff  WB3JFS





- Original Message - 
From: Robert Bruninga bruni...@usna.edu
To: 'Jeff Yanko' wb3...@cox.net; amsat-bb@amsat.org
Sent: Friday, February 26, 2010 5:31 AM
Subject: RE: [amsat-bb] Planet Pseudo-Keps


 Are there any  pseudo-keps for the planets?

 Actually, the word planet comes from the meaning wanderers
 because that is what stumped the early astronomers thousands of
 years ago.  They do not have regular motion about Earth... And
 Copernicus finally figured it out... They rotate around the sun.

 Bob

 


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[amsat-bb] Re: Planet Pseudo-Keps

2010-02-27 Thread Nigel Gunn G8IFF/W8IFF
You saying that if I lived on another planet or in another star system then my 
satellites wouldn't have keps and I 
couldn't use my software to track them?

That sounds rediculous.

On 27-Feb-10 09:43, Jeff Yanko wrote:


 Since the planets revolve around the Sun ,and not the Earth, there can't be
 any Keps.  Keps are based on the Earth being the center of an orbiting
 object.
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[amsat-bb] Re: Planet Pseudo-Keps

2010-02-27 Thread Bob Bruninga
 Since the planets revolve around the Sun,
 and not the Earth, there can't be any Keps.  
 Keps are based on the Earth being the 
 center of an orbiting object.

 You're saying that if I lived on another planet 
 or in another star system then my satellites 
 wouldn't have keps and I couldn't use my 
 software to track them?... That sounds rediculous.

Yep. keps (as we use the term here regularly) either in AMSAT format or in 
NASA two-line format are just inputs to an Earth orbit propogator that 
predicts where a satellite is around Earth based on the laws of physics.

If you lived on Mars, and had a Mars Orbit Propogator then you could download 
Martian Keps from the Martians and track Martian satellites.  But the Martian 
tracking program would not be able to track earth satellies, just as ours Earth 
based programs cannot track theirs.  Because the size and mass of Mars is 
different from Earth, so the propogators have to be different... or something 
like that.  I'm on the limit of my meager knowledge here...

Bob, Wb4APR


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[amsat-bb] Re: Planet Pseudo-Keps

2010-02-27 Thread Auke de Jong, VE6PWN
I would have to guess that this is entirely possible otherwise Mars and Moon 
missions would be shots-in-the-dark.  The software to do this is most likely 
completely different from that which predicts simple satellites around one 
planet.  Tracking other planets relative to ours would be more like 
predicting angles and velocities from one LEO to another LEO.  The software 
would need to contain the keps of the solar system, and then give results 
from the perspective of one of the satellites.  This software probably 
already exists, but in the proprietary domain.

On second thought, the software that runs the fully-automated personal 
telescopes already does most of this, except for the relative velocity part.

73's
Auke

- Original Message - 
From: Jeff Yanko wb3...@cox.net
To: amsat-bb@amsat.org
Sent: Friday, February 26, 2010 2:09 AM
Subject: [amsat-bb] Planet Pseudo-Keps
  Which brings to question.  Are there any pseudo-keps for the
 planets?


 73,

 Jeff  WB3JFS

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[amsat-bb] Re: Planet Pseudo-Keps

2010-02-27 Thread Stephen Melachrinos
Feb 27, 2010 08:43:51 AM, bruni...@usna.edu wrote:

 Since the planets revolve around the Sun,
 and not the Earth, there can't be any Keps. 
 Keps are based on the Earth being the 
 center of an orbiting object.

 You're saying that if I lived on another planet 
 or in another star system then my satellites 
 wouldn't have keps and I couldn't use my 
 software to track them?... That sounds rediculous.

Yep. keps (as we use the term here regularly) either in AMSAT format or in 
NASA two-line format
are just inputs to an Earth orbit propogator that predicts where a satellite 
is around Earth based
on the laws of physics.

If you lived on Mars, and had a Mars Orbit Propogator then you could 
download Martian Keps 
from the Martians and track Martian satellites. But the Martian tracking 
program would not be able 
to track earth satellies, just as ours Earth based programs cannot track 
theirs. Because the size 
and mass of Mars is different from Earth, so the propogators have to be 
different... or something 
like that. I'm on the limit of my meager knowledge here...


Bob (and Nigel) -

That's pretty accurate. Although the laws of physics apply universally around 
all the planets, the specific implementations of orbit mechanics software are 
location dependent. You gave one example--size and mass of the Earth vs Mars. 
Other examples are the oblateness of the planet (how flattened at the poles is 
Mars vs Earth) and the effects of other objects such as the moon and other 
planets. (The effects of the earth's moon on an earth-orbiting satellite will 
be different from the effects of Deimos and Phobos on a Mars-orbiting 
satellite.)

Although the equations are all the same, most programs (that are publicly 
distributed) assumes the earth as the core body, and embeds those assumptions 
into the software. I think STK (Satellite Tool Kit) by Analytical Graphics may 
have the ability to analyze non-Earth geometries, but it's hardly within the 
realm of amateurs. (A full-up version costs something like US$50,000.)

Steve
W3HF
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[amsat-bb] NASA cubesats...

2010-02-27 Thread Rocky Jones

http://www.spaceref.com/news/viewpr.html?pid=30294

there are going to be more ballast payloads particularly as commercial ops to 
the space station gens up.  Just saw a thing today where almost all the folks 
who are planning to do commercial ops are looking at ballast rides.

Robert G. Oler Life member AMSAT ARRL
  
_
Your E-mail and More On-the-Go. Get Windows Live Hotmail Free.
http://clk.atdmt.com/GBL/go/201469229/direct/01/
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[amsat-bb] Re: Planet Pseudo-Keps

2010-02-27 Thread Ken Ernandes
Your statement is correct, however there is an issue of context.  Most
satellite tracking software uses Simplified General Perturbations No. 4
(SGP4) as an orbit propagator.  SGP4 is one of several orbit propagation
algorithms that presume the Earth to be the central attracting body (as both
origin and major attracting mass).  As such, the associated Keplerian
elements are in the context of an Earth-orbiting satellite as are the
corresponding output positions and velocities.  This is a convenient
simplifying assumption for Earth-orbiting satellites and also since Earth
station coordinates use the center of the Earth as the origin.

Certainly, there are orbit propagation (and ephemeris interpolation) methods
that have a different (or a flexible choice of) attracting body (and
therefore a different origin and central mass).  In using such an algorithm,
the software must also (1) know the mass of the central attracting body, (2)
compute the Earth's position relative to the origin (the attracting body)
and (3) also determine its orientation relative to (for example) the Sun's
coordinate system.  This requires an additional translation (i.e., vector
subtraction) and a re-orientation (i.e., coordinate transformation).  These
are fairly simple to code into a library and thus simple to use.  However,
the software needs to have that additional logic already embedded.

I do not know of a method in which the Keplerian elements of a planet
orbiting the Sun could be used to produce any sort of meaningful answer in
software that propagates orbit using an Earth-centered propagator.  Indeed,
there's nothing wrong with the physics, but one must pay attention to the
simplifying assumptions underlying the implemented algorithms.





-Original Message-
From: amsat-bb-boun...@amsat.org [mailto:amsat-bb-boun...@amsat.org] On
Behalf Of ve4yz
Sent: Saturday, February 27, 2010 11:41 AM
To: amsat-bb@amsat.org
Subject: [amsat-bb] Re: Planet Pseudo-Keps

Keplerian Elements have nothing to do with the Earth.   To say it only
applies to earth orbiting objects would be like saying Newton's laws of
motion only apply to the earth.

They are mathematical descriptions of the motion of one body orbiting
another in an unperturbed orbit using the 6 degrees of freedom of the
orbiting body - i.e the 6 key elements of the keps. 

They predate computers and software; circa 1605. 

This not to say that they are universally applicable.  Larger or smaller as
in galactic or subatomic with perturbed orbits - all bets are off. 



 

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[amsat-bb] working FO-29

2010-02-27 Thread Bill Dzurilla
I tried to work FO-29 for the first time since it started working again but 
must be doing something wrong.  I could hear several stations loud and clear 
but could not hear my own downlink.  My radio is working fine with the other 
sats, so it must be someone particular to FO-29.  Did perhaps the uplink change 
frequency or something?

73, Bill NZ5N


  
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[amsat-bb] Re: working FO-29

2010-02-27 Thread PE0SAT

On Sat, February 27, 2010 18:44, Bill Dzurilla wrote:

Hi Bill,

 I tried to work FO-29 for the first time since it started working again
 but must be doing something wrong.  I could hear several stations loud
 and clear but could not hear my own downlink.  My radio is working fine
 with the other sats, so it must be someone particular to FO-29.  Did
 perhaps the uplink change frequency or something?


I don't now if you use tracking software,
but here is my FO-29 entry for SatPC32

FO-29,435850,145950.95,USB,LSB,REV,0,0,Transponder
FO-29,435795,0,CW,CW,NOR,0,0,Beacon


 73, Bill NZ5N


73 Jan - PE0SAT


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[amsat-bb] Re: Planet Pseudo-Keps

2010-02-27 Thread Joe Fitzgerald
Auke de Jong, VE6PWN wrote:

 On second thought, the software that runs the fully-automated personal 
 telescopes already does most of this, except for the relative velocity part.

   
The US government will do that for us via the JPL HORIZONS tracking 
system http://ssd.jpl.nasa.gov/?horizons  The data below show that as 
this being written I should point my antennas to the south, a little 
less than half way up from horizon to my zenith.  Jupiter is moving away 
from me at about  six and a half kilometers per second, and a dit 
leaving my keyer will take the better part of an hour to reach it's target.

No charge to use this, US hams pay for this with our taxes.  That being 
said you Canadians are welcome to send me cash gifts, and I will be glad 
to pay the appropriate US income tax on it!

-Joe KM1P

***
 Revised: Dec 17, 2009  Jupiter 599
 
 PHYSICAL DATA (updated 2009-Jan-28):
  Mass (10^24 kg)   =  1898.13+-.19   Density (g/cm^3)   =  1.326
  Equat. radius (1 bar) = 71492+-4 km Polar radius (km)  = 66854+-10
  Volumetric mean radius= 69911+-6 km Flattening =  0.06487

  Rotation period   = 9h 55m 29.685s  Rot. rate(10^-4 rad/s) =  1.75865
  m = w^2a^3/GM =  0.089195   Hydrostatic flat., fh  =  0.06509
  Inferred rot. period  =  9.894+-0.02 hr ks = 3*J2/m=  0.494
  Mom. of inert. I/MRo^2=  0.254  I/MRo^2 (upper bound)  =  0.267 
  Rocky core mass (Mc/M)=  0.0261 Y factor (He/H ratio)  =  0.18+-0.04

  GM (km^3/s^2) = 126,686,511 GM 1-sigma (km^3/s^2)  = +-100
  Equ. grav, ge (m/s^2) = 24.79   Pol. grav, gp (m/s^2)  = 28.34

  Geometric albedo  =  0.52   Visual magnitude V(1,0)= -9.40
  Vis. mag. (opposition)= -2.70   Obliquity to orbit =  3.12 deg
  Sidereal orbit period = 11.862615 yrSidereal orbit period  = 4332.820 d
  Mean daily motion = 0.0831294 deg/d Mean orbit velocity= 13.0697 km/s

  Atmos. temp. (1 bar)  = 165+-5 KHeat flow/mass (x10^7) = 15 erg/gm*s
  Planetary Solar Const =  50.5 W/m^2 Dipole tilt/offset = 9.6deg/0.1Rp 
  Escape velocity (km/s)=  59.5   Mag.dip.mom(gauss-Rp^3)= 4.2 
  Aroche(ice)/Rp=  2.76   Hill's sphere rad. Rp  = 740
***
 
 
***
Ephemeris / WWW_USER Sat Feb 27 10:15:04 2010  Pasadena, USA / Horizons
***
Target body name: Jupiter (599)   {source: JUP230}
Center body name: Earth (399) {source: DE405}
Center-site name: (user defined site below)
***
Start time  : A.D. 2010-Feb-10 17:00:00. UT  
Stop  time  : A.D. 2010-Feb-10 20:00:00. UT  
Step-size   : 5 minutes
***
Target pole/equ : IAU_JUPITER {East-longitude -}
Target radii: 71492.0 x 71492.0 x 66854.0 km  {Equator, meridian, pole}
Center geodetic : 288.845300,42.2925472,49.999402 {E-lon(deg),Lat(deg),Alt(km)}
Center cylindric: 288.845300,4762.18349,4303.3386 {E-lon(deg),Dxy(km),Dz(km)}
Center pole/equ : High-precision EOP model{East-longitude +}
Center radii: 6378.1 x 6378.1 x 6356.8 km {Equator, meridian, pole}
Target primary  : Sun {source: DE405+DE408}
Interfering body: MOON (Req= 1737.400) km {source: DE405}
Deflecting body : Sun, EARTH  {source: DE405}
Deflecting GMs  : 1.3271E+11, 3.9860E+05 km^3/s^2  
Atmos refraction: NO (AIRLESS)
RA format   : HMS
Time format : CAL 
RTS-only print  : NO   
EOP file: eop.100226.p100520   
EOP coverage: DATA-BASED 1962-JAN-20 TO 2010-FEB-26. PREDICTS- 2010-MAY-19
Units conversion: 1 AU= 149597870.691 km, c= 299792.458 km/s, 1 day= 86400.0 s 
Table cut-offs 1: Elevation (-90.0deg=NO ),Airmass (38.000=NO), Daylight (NO )
Table cut-offs 2: Solar Elongation (  0.0,180.0=NO )   
*
 Date__(UT)__HR:MN Azi_(a-appr)_Elev dAZ*cosE d(ELV)/dt  APmag  S-brt   
 delta  deldot   1-way_LT
*
$$SOE
 2010-Feb-10 17:00 *m  163.9922  35.9868   867.85184.19  -2.02   5.31 
8.8974883901E+08   6.3227121  49.464711
 2010-Feb-10 17:05 *m  165.4872  36.2310   871.25167.40  -2.02   5.31 
8.8975073674E+08   6.3287606 

[amsat-bb] W7LRD 5/4 RPT WORKED AGAIN 2E1EUB

2010-02-27 Thread paul robinson
W7LRD 5/4 RPT IO92BX NICE QSO AGAIN VIA AO7  BOB    IM STILL LOOKING WEST 
COAST GUYS!!! CALL ME PLEASE OR ARRANGE A SKED DE PAUL 2E1EUB


  
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[amsat-bb] 2M1EUB/P QRV N.E.SCOTLAND 20/3/10

2010-02-27 Thread paul robinson
2M1EUB/P WILL BE QRV FROM N.E. SCOTLAND FROM 20/03/10 ON ALL BIRDS FOR 7 DAYS 
CHQ OUT 2M1EUB LISTING ON QRZ FOR MORE INFO ..DE PAUL 2E1EUB


  
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[amsat-bb] Recording, AO-51 V/S 23:25 pass?

2010-02-27 Thread George Henry
Anybody have a recording of the 23:25 pass of AO-51 in mode V/S?  I was so 
busy juggling two radios  waving a hand-held K5GNA downconverter (w/ corner 
reflector) around, I forgot to write down the call of the station in EM13 
that I worked...

And thanks Allen, Angelo, and Leo for the contacts!!  I haven't been on V/S 
since Field Day a couple of years ago, forgot how un-crowded it is!



George, KA3HSW 

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[amsat-bb] ANS-059 AMSAT Weekly Bulletins

2010-02-27 Thread Lee McLamb
AMSAT NEWS SERVICE
ANS-059

ANS is a free, weekly, news and information service of AMSAT North America, The
Radio Amateur Satellite Corporation. ANS reports on the activities of a
worldwide group of Amateur Radio operators who share an active interest in
designing, building, launching and communicating through analog and digital
Amateur Radio satellites.

Please send any amateur satellite news or reports to:

ans-edi...@amsat.org


In this edition:
* Amateur Satellite Presentation at Edison Amateur Radio Network Meeting
* AMSAT Activities at the Greater Houston Hamfest
* AMSAT Preparing for Hamvention 2010
* Indonesian Amateur Radio Satellite update
* ARISS Status - 22 February 2010


SB SAT @ AMSAT $ANS-059.01
Amateur Satellite Presentation at Edison Amateur Radio Network Meeting

AMSAT News Service Bulletin 059.01
  From AMSAT HQ SILVER SPRING, MD.
February 28, 2010
To All RADIO AMATEURS
BID: $ANS-059.01

[Note: times listed are for the local Pacific time zone]

AMSAT area coordinator Clint Bradford, K6LCS, will be presenting his 'Working
Amateur Satellites With Your HT' multimedia 
session at the March 3, 2010 meeting
of the Edison Amateur Radio Network. All are welcome to attend.

Tentatively, we have a pass of AO-51 at 5:40PM before the meeting, Clint
reports. I'll be working the satellite from the AQMD parking lot if you'd like
to show up a few minutes early.

The club meets at the Diamond Bar AQMD building, 
21865 Copley Drive, Diamond Bar
CA  91765 - close to the 57/60 freeway interchange. Meeting starts at 6PM.

Attendees are encouraged to download Clint's four-page tutorial and radio
programming matrix before the meeting from ... http://www.work-sat.com

And Clint welcomes pre-presentation questions - call him at 909-241-7666, or
send email to ... cl...@clintbradford.com

[ANS thanks Clint, K6LCS, for the above information]

/EX


SB SAT @ AMSAT $ANS-059.02
AMSAT Activities at the Greater Houston Hamfest

AMSAT News Service Bulletin 059.02
  From AMSAT HQ SILVER SPRING, MD.
February 28, 2010
To All RADIO AMATEURS
BID: $ANS-059.02

Greater Houston Hamfest 2010 in Rosenburg, TX will feature an AMSAT booth,
technical presentation and satellite demos.  Second prize drawing at Hamfest
will be for Kenwood F6A HT with Arrow antenna and duplexer.  Allen Mattis N5AFV
 Andy MacAllister W5ACM are organizing the AMSAT activities.  Listen for
special event callsign, KK5W.

[ANS thanks Allen, N5AFV, for the above information]

/EX


SB SAT @ AMSAT $ANS-059.03
AMSAT Preparing for Hamvention 2010

AMSAT News Service Bulletin 059.03
  From AMSAT HQ SILVER SPRING, MD.
February 28, 2010
To All RADIO AMATEURS
BID: $ANS-059.03

The AMSAT team is preparing for the 2010 Dayton Hamvention AMSAT Booth and
activities.  We are updating information about the AMSAT presence at Dayton
on the AMSAT Web site, follow the left hand navigation to get to the AMSAT
Hamvention area.  Those wishing to stay with the AMSAT contingent and
volunteering to work on booth setup/take down or in the booth itself are
invited to contact Martha to make your hotel reservations.  Additional
information about the hotel can be found under the Dayton Hotel 2010 link.
The Friday night AMSAT/TAPR Banquet will be at the same location as the
last three years, the Kohler Banquet Center.  The menu has been selected and
posted on the AMSAT/TAPR Banquet 2010 link.  TAPR will be selecting the
speaker for the banquet this year.
The team is looking forward to displaying AMSAT accomplishments, new
merchandise and talking with our members during the May 14-16, 2010 event.

[ANS thanks Gould, WA4SXM, for the above information]

/EX


SB SAT @ AMSAT $ANS-059.04
Indonesian Amateur Radio Satellite update

AMSAT News Service Bulletin 059.04
  From AMSAT HQ SILVER SPRING, MD.
February 28, 2010
To All RADIO AMATEURS
BID: $ANS-059.04

Wisnu Widjaja YBØAZ brings the latest news on the two new Indonesian
Amateur Radio satellites, LAPAN-ORARI and LAPAN-A2 which are planned
to launch in 2011. ORARI is the Organisasi Amatir Radio Indonesia.

LAPAN-ORARI will carry a 5 watt output FM voice transponder with a
435.880 MHz uplink and 145.880 MHz downlink as well as an APRS Digi-
peater on 145.825 MHz. It will also carry a green light laser for
attitude determination.

It is planned to be launched from India into a 650km orbit with low
(8 degree) inclination as a secondary payload with Megha-Tropique.

LAPAN-A2 will use S band (non amateur frequency) for video surveil-
lance and the amateur frequency 437.425 MHz for telemetry.

Wisnu Widjaja YBØAZ was the responsible operator on the frequency
coordination request for the two satellites submitted to the IARU
Amateur Satellite Frequency Coordination panel which was approved
on December 23, 2009.

Work on LAPAN-ORARI and LAPAN-A2 satellites is currently at the
stage of assembly and testing of components.

More information is available on these satellites at
http://www.lapan.go.id
http://www.orari.or.id
http://www.amsat-id.net

[amsat-bb] Wisp Keying Multipsk - Another go for Pacsat with software.

2010-02-27 Thread Nader Omer
Hi All
 
Another go for Pacsat with software.
This time  Wisp with Multipsk ver 4.16

Wisp Keying Multipsk via VSPE virtual connector port .
So far TX line was testing.

Wisp--Multipsk--soundcard
 
Setup
Create a Connector virtual com using VSPE software
Wisp --com 1
Multipsk serial port for kiss -- com 1
On Multipsk TX/RX screen choose--Packet APRS
On Multipsk TX/R screen click kiss icon.
Run a pass!
Click fill.
MSPE will send a packet to Multipsk TX/RX screen
and through the soundcard.
 
Again I'm waiting for a bird .
 
For more info and Movie see
http://st2nh-blogger.blogspot.com/2010/02/wisp-keying-multipsk.html
 
For my previous Wisp MixW experiments see.
http://st2nh-blogger.blogspot.com/2010/02/pacsat-with-out-hardware-tnc.html
 
http://st2nh-blogger.blogspot.com/2010/02/wisp-keying-mixw-direct-via-virtual.html
 
 
73's Nader


  
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