[amsat-bb] Re: Kick motors on Oscars: How does attitude controlwork?

2013-09-23 Thread i8cvs
Hi Peter,DB2OS

If I well remember in addition with the Magnetorquing ,AO40 
was equipped with a 3 axis X-Y-Z stabilization wheel/EPU 
acting as gyroscopes that never where used except one time
I remember to have seen on the P3T TLM the wheels were
tested rotating for a short time at a very low numbar of turns
... or I am wrong ?

Why the 3 axis stabilization wheel/EPU whre never used on
AO40 ?   

Thanks for your answere.

73 de

i8CVS Domenico

- Original Message -
From: Peter Guelzow peter.guel...@kourou.de
To: amsat-bb@amsat.org
Sent: Sunday, September 22, 2013 11:21 PM
Subject: [amsat-bb] Re: Kick motors on Oscars: How does attitude
controlwork?


 Hi Burns,

 yes - all Phase 3 satellites use Magnetorquers to control attitude
 during perigee. They were pulsed by the IHU on-board computer which was
 running a model of the physics and orbital dynamics to trigger the
 correct coils at the right moment.   This Timing was synchronized with
 the Sun sensor...   indeed P3 spacecrafts are Spin stabilized...
 There was no feedback. Command stations did some calculations based on
 Earth and Sun sensor data, but once calibrated the system worked quite
 smoothly and predictable...
 For the motor burns, the attitude was indeed determined by the Sun and
 Earth sensors and several times corrected until the perfect attitude was
 achieved.. this took a few days.
 Basically a very simple system was simple physics involved...

 73s Peter


 On 22.09.2013 22:19, Burns Fisher wrote:
  There has been a lot of discussion about AO-10, 13, and 40 (and maybe
  others) with various kinds of apogee kick motors (and inclination
  changers etc).  Rather than fanning any flames, I just want to ask a
  question: If you have a motor of a few hundred Newtons, how to
  you keep the attitude stable during the burn?  
  For that matter, how do you get the attitude correct for the start
  of the burn?  I would not think that electromagnets operating against
  the earth's magnetic field would have enough power with
  such a large motor.  
  Obviously it depends on the balance of the satellite relative to the
  position of the kick motor, but still...was the balance really good 
  enough to allow magnetic attitude control?
  Was it active (i.e. with feedback)?  Does that imply a rate gyro?
  (No MEMS then, I suppose).
 
  Thanks in advance for the technical history lesson...
 
  73,
 
  Burns W2BFJ


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[amsat-bb] Re: Kick motors on Oscars: How does attitude controlwork?

2013-09-23 Thread don

Hi,

After a long absence I decided to check out the AMSAT mailing list again.

It's been on my spam list for some time now, (mainly because of the 
insane FM square collecting posts)but I thought it time to check again. 
Amazingly I now find real technical discussions being carried on, is 
this now normal? could some one reply to the affirmative I may even 
find some funds to rejoin amsat if the board now reflects the 
experimental and technical pursuits of real satellite enthusiasts.
Please no more FM sats. I like beep sats and enjoy getting data from 
them.

Don.
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[amsat-bb] k8bl road trip

2013-09-23 Thread k4feg

Here is the Itinerary for/*K*//**//*8BL's road trip starting today:*/

Be sure to listen for Bob on all satellites!

Below is the email Bob sent me:


/*Here is my plan for the week of 9/23-9/27.*/
/**/
/**//**/
/**/
/*I'll be driving around Lake Huron and activating as many of the
Grids I pass through as possible. On Monday 9/23 I'll be headed north from
Detroit and hit EN84, 85, 75,  76, but I may make it to EN77/87 by late*/
/**/
/*afternoon depending on speed  traffic. On Tuesday 9/24 my plan is to 
quickly

go through EN76  77 to hit rare EN87 and back down through EN77, 76
and into EN86. On Wednesday 9/25 I'll be in EN96 and go for rare EN97
and head down into EN95. Thursday 9/26 will take me through FN05, 04
and into EN94. On Friday 9/27 I expect to be in EN94, 93  92. All of this*/
/**/
/*is flexible based on road situations as they arise, but my goal is to 
activate*/

/**/
/*as many of these Grids as possible.

By Saturday 9/28 my plan to to just dead-head back to my QTH in EN91.

Hope to work a lot of the Grid Chasers on my journey!*/
/**/
/**//**/
/**/
/*Frank, please try to get this on Starcom  AMSAT tonight if possible so*/
/**/
/*folks will know I'll be available.

Good Luck Everyone!

*/73 ALL FRM
STARCOM DIV of the GGG
K4FEG
/The Commander
GGHQ: EM55aj84ta

...no grid left behind...
/
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[amsat-bb] 50+ Years Of Space Exploration

2013-09-23 Thread B J
http://edudemic.com/wp-content/uploads/2012/08/50-years-exploration-huge.jpg

73s

Bernhard VA6BMJ@ DO33FL
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[amsat-bb] Re: Phase 3

2013-09-23 Thread Robert McGwier
This I can say, for a fact, is not true.  PROFESSIONALS did the fueling and
safing as was required by contractual arrangements ahead of time.

Eye witness testimony given to me says there was an argument about what to
do about the RBF plug.  Extenuating circumstances, a nearly perfect storm
of them,  including a not really clear coloration and several other
factors caused the decision to be taken not to remove it.

But one thing is absolutely clear.  AMSAT personal were NOT responsible for
fueling and safing.  One or more participated but in red hand mode as in,
if you touch, your hand will be slapped until it is red.

http://n4hy.smugmug.com/AMSAT/AO40-Phase-3D/010-Final-Assembly/2109994_HNF8Hn#!i=109042686k=dShmr5K

It was NOT as clear as you make it out as you can see and it was most
decidedly not firey red and clear as to what to do.

Where things are clear,  they were and are marked clearly:

http://ukamsat.files.wordpress.com/2013/02/ao-40.jpg

The deal is,  AO-40 flew.  It gave quite a long period of interesting
operation.  It did not attain all of its goals and was an unbelievable
complex achievement from the birth of the concept:

http://n4hy.smugmug.com/AMSAT/AO40-Phase-3D/001-Marburg0590/2107966_HX26gC#!i=108935294k=ssKW2Fblb=1s=A

until its death, it was and remains AMSAT (all versions and hyphens)
greatest achievement.






On Sat, Sep 21, 2013 at 10:19 PM, R Oler orbit...@hotmail.com wrote:

 The people installing them and safing them and all the other things were
 mostly not rocket scientist that is why somewhere on AO-40 there is a
 remove before flight what we call in the business flag flying  RGO

 Sent from my iPad

  On Sep 22, 2013, at 1:55 AM, Angus McLeod amcl...@caribsurf.com
 wrote:
 
  As far as I know, the kick-motors used on the Phase-3 birds were NOT
 cardboard tubes packed with homemade gunpowder.  They were commercial grade
 motors obtained from the commercial aerospace industry.  If I am wrong
 about this, and someone can jump in with facts, I'd be glad to hear.
 
 
  On 09/21/2013 05:48 AM, Gordon JC Pearce wrote:
  On Fri, Sep 20, 2013 at 11:23:29PM +0600, R Oler wrote:
  While anything is possible I will be very surprised (pleasntly) if
 there is another amateur radio satellite with a liquid propulsion system
 that is managed by any amateur group that gets a ride into any sort of HEO
 transfer orbit.Ion engines might be different but after AO-40 and its
 propulsion issues the days of amateurs playing with rocket engines on
 commercial flights I suspect is over.
  This is something I've often wondered about.  Oh hi, commercial rocket
 company, can we stick our homebrewed rocket into your billion dollar
 vehicle?
 
  When people with more oil than weapons stuff some mix of chemicals into
 a tube and crimp the end shut it's called an Improvised Explosive Device.
  We're supposed to somehow convince someone to let us tack our semitested
 bomb onto their flight?  I doubt they're going to go for it...
 
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-- 
Bob McGwier
Owner and Technical Director, Allied Communication, LLC
Professor Virginia Tech
Senior Member IEEE, Facebook: N4HYBob, ARS: N4HY
Faculty Advisor Virginia Tech Amateur Radio Assn. (K4KDJ)
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[amsat-bb] Re: SatPC32 Registration

2013-09-23 Thread Alan
Carl,

According to the records, you ordered it late Thursday evening.  As you know, 
we have a tiny (1)
office staff, and the program registration process is done manually rather than 
automagically.  It
sometimes take a few days to process, depending on many issues.  This is 
mentioned on the web site.
Mondays are particularly brutal.  The registration will be along shortly.

73s,

Alan
WA4SCA
AMSAT Store Stock Boy



-Original Message-
From: amsat-bb-boun...@amsat.org 
[mailto:amsat-bb-boun...@amsat.org] On Behalf Of carl creamer
Sent: Monday, September 23, 2013 1:05 PM
To: amsat-bb@amsat.org
Subject: [amsat-bb] SatPC32 Registration

I need some advice on how to solve this.
I downloaded  and installed SatPC32 V.12.8b a few weeks ago 
and got it up and working as it should.It is a cool program.
I also  ordered the Registration on paypal last week , but 
have yet to receive the registration information email.
I sent an email and called the 1-888 number and so far no response.
Any suggestion on how to resolve this would be greatly appreciated.
Thanks
Carl
WQ6C
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[amsat-bb] Re: SatPC32 Registration

2013-09-23 Thread Martha
To All - The date on the PayPal form I downloaded today was Saturday, Sept
21.  I sent the password to Carl around 30 minutes ago.  One day turn
around for a 1 person office is pretty good!


On Mon, Sep 23, 2013 at 4:20 PM, Alan wa4...@gmail.com wrote:

 Carl,

 According to the records, you ordered it late Thursday evening.  As you
 know, we have a tiny (1)
 office staff, and the program registration process is done manually rather
 than automagically.  It
 sometimes take a few days to process, depending on many issues.  This is
 mentioned on the web site.
 Mondays are particularly brutal.  The registration will be along shortly.

 73s,

 Alan
 WA4SCA
 AMSAT Store Stock Boy



 -Original Message-
 From: amsat-bb-boun...@amsat.org
 [mailto:amsat-bb-boun...@amsat.org] On Behalf Of carl creamer
 Sent: Monday, September 23, 2013 1:05 PM
 To: amsat-bb@amsat.org
 Subject: [amsat-bb] SatPC32 Registration
 
 I need some advice on how to solve this.
 I downloaded  and installed SatPC32 V.12.8b a few weeks ago
 and got it up and working as it should.It is a cool program.
 I also  ordered the Registration on paypal last week , but
 have yet to receive the registration information email.
 I sent an email and called the 1-888 number and so far no response.
 Any suggestion on how to resolve this would be greatly appreciated.
 Thanks
 Carl
 WQ6C
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 satellite program!
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-- 
73- Martha
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[amsat-bb] Another Delay For Cygnus

2013-09-23 Thread B J
http://www.spaceflightnow.com/antares/cots1/130922delay/#.Uj8Tl9IwkQM
http://www.parabolicarc.com/2013/09/23/cygnus-rendezvous-postponed-crew-arrrival/
http://www.americaspace.com/?p=42942

73s

Bernhard VA6BMJ @ DO33FL
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[amsat-bb] Fw: Delfi C3 Close Approach Notification

2013-09-23 Thread Peter Portanova
FYI

73's WB2OQQ

Sir/Ma'am,

The United States Joint Space Operations Center (JSpOC) has identified a
predicted conjunction between Delfi C3 (SCC# 32789) and SCC# 38013.

Primary Object: Delfi C3 (SCC# 32789)
Secondary Object: SCC# 38013
Time of Closest Approach: 26 SEP 2013 02:05 UTC

Overall miss distance: 796 meters
Radial (dU) miss distance: -177 meters
In-Track (dV) miss distance: 760 meters
Cross-track (dW) miss distance: -158 meters

Primary Radial Error (U): 24 meters
Primary In-track Error (V): 1443 meters
Primary Cross-track Error (W): 7 meters

Secondary Radial Error (U): 11 meters
Secondary In-track Error (V): 703 meters
Secondary Cross-track Error (W): 5 meters


Very Respectfully,

JSpOC Orbital Protection Team
Joint Space Operations Center

NO WARRANTIES: The United States provides the enclosed Space Situational
Awareness (SSA) services or information as is and makes no warranty,
either express or implied, as to the condition or suitability of the
information and services, nor its fitness for a particular purpose.

IMMUNITY: The United States, any agencies and instrumentalities thereof, and
any individuals, firms, corporations, and other persons acting for the
United States, shall be immune from any suit in any court for any cause of
action arising from the provision or receipt of SSA services or information,
whether or not provided in accordance with 10 USC 2274, or any related
action or omission.
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[amsat-bb] SatPC32 Registration

2013-09-23 Thread carl creamer
I need some advice on how to solve this.
I downloaded  and installed SatPC32 V.12.8b a few weeks ago and got it up and 
working as it should.It is a cool program.
I also  ordered the Registration on paypal last week , but have yet to receive 
the registration information email.
I sent an email and called the 1-888 number and so far no response.
Any suggestion on how to resolve this would be greatly appreciated.
Thanks
Carl
WQ6C
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[amsat-bb] Story About Buran

2013-09-23 Thread B J
http://arstechnica.com/science/2013/09/the-life-and-death-of-buran-the-ussr-shuttle-built-on-faulty-assumptions/

73s

Bernhard VA6BMJ @ DO33FL
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[amsat-bb] Re: Phase 3

2013-09-23 Thread Paul Stoetzer
I recently obtained a copy of the 1990 edition of Martin Davidoff's
Satellite Experimenters' Handbook and as I was browsing through the book, I
came across a passage on page 4-9 about the difficulties with UO-11, that's
very relevant to the ongoing debate about the lack of Phase 3 satellites:

If there's a message here, it's that taking part in the amateur satellite
program is not for the faint-hearted. Setbacks and barriers will always be
part of the picture. And, the most rewarding successes will probably come
from employing ingenuity and tenacity to overcome the 'impossible' hurdles.

73,

Paul Stoetzer, N8HM
Washington, DC (FM18lv)


On Sun, Sep 22, 2013 at 7:17 PM, mlengrues...@aol.com wrote:



 Hi Dan,

 OSCAR-10 (P3-B) used the same 400N engine as OSCAR-13 (P3-C)  and
 OSCAR-40 (P3-D).
 For P3-E we have a 200N motor from EADS Astrium, the  same one which is
 used on the European ATV...

 I was AMSAT P3-A  (planned to be OSCAR-9) which used a solid propellant
 apogee  kick-motor.
 It's under the water near the cost of french Guiana..   RIP

 You can find an very good article  here:
 http://www.ka9q.net/AMSAT-Tech-Journal-2.pdf
 See page  8..15

 Rest assured, the PFA and propulsion system was qualified according  to
 highest commercial standards by commercial companies. Thus in no  way
 there would be any risk to the launcher or other payloads. This  also
 includes several levels of safety borders in the hardware design and  in
 the software.   The launch agencies have there own specialized  personal
 to review all the details...Without that, nobody would  have launched
 any of the P3 satellites !!!
 What happened to  AO-40 later on after orbit injection and after
 activating the systems is a  completely different matter and did not
 present any risk to the launcher at  any time!



 Michael R. Lengruesser, DD5ER

 AMSAT-DL e.V.
 -- International Satellites for Communication,
 Science and Education --
 mlengrues...@amsat-dl.org
 http://www.amsat-dl.org



 In einer eMail vom 22.09.2013 21:07:08 Westeuropäische Sommerzeit schreibt
 n8...@usa.net:

 The apogee motors for OSCAR-10,and OSCAR-13 were solid  propellant
 400 Newton trust motors donated to AMSAT-DL by the  Messerschmitt
 Aerospace
 Company in Germany.

 Only Phase 3A  had a solid fuel motor. AO-10 and AO-13 had liquid fuel
 bi-propellent  motors the same as AO-40. No matter how well designed they
 are,
 they still  have the potential to blow up the entire launch stack if
 something
 goes  wrong. Since Dick Daniels is no longer with us, the knowledge has
 been
 lost  and we will not be launching any more of these in the future.

 Dan  Schultz  N8FGV


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[amsat-bb] Re: Kick motors on Oscars: How does attitude control work?

2013-09-23 Thread Bryce Salmi
Found this intersting web page:

http://www.isispace.nl/cms/index.php/projects/nks

Bryce
KBL1QC


On Mon, Sep 23, 2013 at 12:46 PM, Burns Fisher bu...@fisher.cc wrote:

 Very interesting stuff.  Thanks to everyone who responded.  Using a model
 rocket engine has occurred to me :-)  I noticed that the smaller ones (A,B)
 tend to peak at 10s of Newtons (presumably to get the model rocket going
 fast enough to be stable after it leaves the launch rod) and then settles
 down to sub-10 Newtons for the rest of the burn (a second or two).  So it
 is quite a whack over a short period for a small bird.  I did not look up
 the higher power size.  It would be interesting and not too difficult to do
 the math to see what kind of a perigee raise would happen if someone fired
 one of these on a 3U cubesat of modest mass in GTO while it was at apogee.

 Don, there is enough interesting stuff to keep me watching the list.  There
 is also a lot of complaining.  We'd love to have you rejoin AMSAT.  Fox-1,
 the upcoming launch, IS an FM bird, but I hope you noticed that the last
 AMSAT bird, ARRISat-1 was indeed a linear.  We need to continue to learn
 and experiment.

 Burns, W2BFJ

 On Sun, Sep 22, 2013 at 5:49 PM, Daniel Schultz n8...@usa.net wrote:
 
   I just want to ask a question:  If you have a motor of a few hundred
   Newtons, how to you keep the attitude stable during the burn?  For
 that
   matter, how do you get the attitude correct for the start of the burn?
  
   Simple question, simple answer: You use the magnetotorquers to point
 the
   spin
   axis in the right direction, check and check again to make sure you got
   that
   right, then use the magnetotorquers again to spin up the satellite at a
   high
   angular rate (maybe 20 RPM). The angular momentum of the spinning
  satellite
   keeps it stable while the motor is firing. The motor thrust must of
  course
   be
   well aligned with the spin axis, but if the thrust vector is not
 perfect,
   the
   spinning satellite tends to even out the small deviation.
  
   One of the recent Cubesats carried high power model rocket engines to
 try
   an
   experimental orbit adjustment. They forgot to spin the satellite and
 the
   Cubesat tumbled wildly as a result of the motor burn. Some of these
  groups
   are
   really lacking in basic physics knowledge (and we are not talking about
  wet
   behind the ears students in that case.)
  
   Dan Schultz N8FGV
  
  
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  --
 
  Message: 7
  Date: Sun, 22 Sep 2013 22:22:11 -0400
  From: Joe Fitzgerald jfitzger...@alum.wpi.edu
  To: AMSAT BB amsat-bb@amsat.org
  Subject: [amsat-bb] Re: Kick motors on Oscars: How does attitude
  control work?
  Message-ID: 523fa5d3.3020...@alum.wpi.edu
  Content-Type: text/plain; charset=ISO-8859-1; format=flowed
 
  On 9/22/2013 4:19 PM, Burns Fisher wrote:
 I would not think that electromagnets
   operating against the earth's magnetic field would have enough power
 with
   such a large motor.
 
  The electromagnets had some oomph  I seem to remember the engineering
  beacon moving in frequency slightly when they switched on ... I don't
  remember if it was because of a sag on the DC bus, or the magnetic field
  affecting the tuned circuits of the transmitter.
 
  But you bring up important points,  if we are to do orbit adjustments,
  we need to do attitude determination and control in addition to getting
  a motor aboard.  No easy feat in a 3U cubesat!
 
  -Joe KM1P
 
 
  --
 
  Message: 8
  Date: Mon, 23 Sep 2013 08:14:44 +0200
  From: i8cvs domenico.i8...@tin.it
  To: Peter Guelzow peter.guel...@kourou.de,  Amsat - BBs
  amsat-bb@amsat.org, Daniel Schultz n8...@usa.net
  Subject: [amsat-bb] Re: Kick motors on Oscars: How does attitude
  controlwork?
  Message-ID: 000901ceb824$34922710$0301a8c0@i8cvs
  Content-Type: text/plain;   charset=iso-8859-1
 
  Hi Peter,DB2OS
 
  If I well remember in addition with the Magnetorquing ,AO40
  was equipped with a 3 axis X-Y-Z stabilization wheel/EPU
  acting as gyroscopes that never where used except one time
  I remember to have seen on the P3T TLM the wheels were
  tested rotating for a short time at a very low numbar of turns
  ... or I am wrong ?
 
  Why the 3 axis stabilization wheel/EPU whre never used on
  AO40 ?
 
  Thanks for your answere.
 
  73 de
 
  i8CVS Domenico
 
  - Original Message -
  From: Peter Guelzow peter.guel...@kourou.de
  To: amsat-bb@amsat.org
  Sent: Sunday, September 22, 2013 11:21 PM
  Subject: [amsat-bb] Re: Kick motors on Oscars: How does attitude
  controlwork?
 
 
   Hi Burns,
  
   yes - all Phase 3 satellites use Magnetorquers to 

[amsat-bb] Odd Question

2013-09-23 Thread MICHAEL
For the longest time I have been wondering how a satellite is placed in
orbit without hitting anything else? I have seen pictures of all the stuff
circling the Earth and it just baffles me how anyone can get anything in
orbit  without hitting anything. Can anyone explain this?

Mike/N8GBU

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[amsat-bb] Re: Odd Question

2013-09-23 Thread Jim Jerzycke
Since the path that the launch vehicle will take is very well defined 
(unless something goes wrong!), and the paths of most objects that would 
intersect this path can be predicted, it becomes a juggling act to get a 
time when the launch vehicle will have a clear path, and your ground 
assets are available.


Since it takes a certain amount of time to get the launch vehicle ready, 
you work backwards from when you know your path will be clear on your 
trajectory to determine when you start your countdown.


The launch provider I work for has several people who do nothing but 
plan things like this, in coordination with USSTRATCOM, NASA, the FAA, 
the European Space Agency, the Russian Space Agency, and all the other 
other launch providers.


In the 9 years I've been doing my part (Communications, Range, and 
Telemetry) we've only had one external hold, and that was caused by 
NASA having to move the ISS a bit because the ISS was going to have a 
close approach of some space junk.


It's called a COLA (COllision Avoidance) hold, and if everybody does 
their planning properly, doesn't usually cause a problem.


One of the things considered is the ascent speed of the launch vehicle, 
as it's going pretty fast during it's passage through various altitudes.


HTH!

73, Jim  KQ6EA


On 09/24/2013 04:22 AM, MICHAEL wrote:

For the longest time I have been wondering how a satellite is placed in
orbit without hitting anything else? I have seen pictures of all the stuff
circling the Earth and it just baffles me how anyone can get anything in
orbit  without hitting anything. Can anyone explain this?

Mike/N8GBU

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[amsat-bb] Re: Odd Question

2013-09-23 Thread Bryce Salmi
This is actually a great question. I've even asked it myself to some
coworkers (in the Guidance, Navigation, and Control department). When it
comes down to it, the space above Earth where satellites orbit is actually
vast. There's a heck of a lot more space than most images showing space
debris will elude to. This is largely because most of those images showing
space junk use dots to represent the pieces we know about. The problem is
that given the scale of the Earth in these images, that tiny dot is
actually MASSIVE compared to the realistic size of even a large satellite.
The truth is that while there's a large amount debris, the chance of
actually hitting anything is pretty small due to the sheer amount of space
the debris is distributed in. The images showing space debris as dots or
other icons are actually pretty poor representations of the space debris
problem (they look cool though). A probability distribution or similar is
what I would imagine as being more useful.

Bryce
KB1LQC


On Mon, Sep 23, 2013 at 9:22 PM, MICHAEL mikef1...@live.com wrote:

 For the longest time I have been wondering how a satellite is placed in
 orbit without hitting anything else? I have seen pictures of all the stuff
 circling the Earth and it just baffles me how anyone can get anything in
 orbit  without hitting anything. Can anyone explain this?

 Mike/N8GBU

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[amsat-bb] Re: Odd Question

2013-09-23 Thread Franklin Antonio

At 09:22 PM 9/23/2013, MICHAEL wrote:

For the longest time I have been wondering how a satellite is placed in
orbit without hitting anything else? I have seen pictures of all the stuff
circling the Earth and it just baffles me how anyone can get anything in
orbit  without hitting anything. Can anyone explain this?


Sure.  Those pictures you've been looking at are not drawn to scale.

The dots representing the satellites should be a lot smaller.  If 
they were, you'd see there's a lot of space out there.


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