Re: [time-nuts] Fwd: CGSIC: FW: The next GPS Launch

2014-07-30 Thread Björn
Its positive that the SVs has exceeded contract design life saving money with 
less launches.

But the launch on failure policy has also delayed the modernization of the 
constellation - even if the last batch of 2R were retrofitted with some new 
signals. I imagine that having SVs sitting in storage for 5+(more?) years also 
has its implications with keeping support contracts etc.

Cheers,
         Björn

div Originalmeddelande /divdivFrån: Magnus Danielson 
mag...@rubidium.dyndns.org /divdivDatum:2014-07-29  20:46  (GMT+01:00) 
/divdivTill: time-nuts@febo.com /divdivRubrik: Re: [time-nuts] Fwd: 
CGSIC: FW: The next GPS Launch /divdiv
/divJohn,

It has delayed the launching of birds, as the old ones does not die of 
quick enough for the planned schematic to maintain 24 birds, instead we 
see 30-32 birds active for many years, and some being off air backups.

On the other hand, it gives more time to adjust the new birds with new 
signals.

Cheers,
Magnus

On 07/29/2014 08:42 PM, John Allen wrote:
 Hi Magnus et al - just FYI: 2 1/2 times the design lifetime is not unusual
 for satellites.  More of the Ham Oscar satellites have exceeded their
 lifetime by that much or more.  (Sorry, no facts handy).

 It saves us USA taxpayers money when they last that long!

 Regards, John K1AE

 Original Message-
 From: time-nuts-boun...@febo.com [mailto:time-nuts-boun...@febo.com] On
 Behalf Of Magnus Danielson
 Sent: Tuesday, July 29, 2014 2:12 PM
 To: Discussion of precise time and frequency measurement
 Subject: [time-nuts] Fwd: CGSIC: FW: The next GPS Launch

 Fellow time-nuts,

 Things will shift in the sky. Lot's of changes.

 SVN-33 is being decommissioned after 17.5 years of operation, with a 7 years
 designed lifetime, that's 2.5 times the operational lifetime, and it's being
 decommissioned in a controlled fashion. Respect.

 Cheers,
 Magnus


  Original Message 
 Subject: CGSIC: FW: The next GPS Launch
 Date: Tue, 29 Jul 2014 17:23:10 +
 From: Civil Global Positioning System Service Interface Committee
 (CGSIC) cg...@cgls.uscg.mil
 Reply-To: cg...@cgls.uscg.mil
 To: cg...@cgls.uscg.mil cg...@cgls.uscg.mil

 All CGSIC:
   The Air Force is set to launch the 7th GPS IIF satellite from Cape
 Canaveral Air Force Station in Florida.

 Delta IV GPS IIF-7 Mission Overview:

 Atlas V GPS IIF-7 Mission Brochure:
 http://www.ulalaunch.com/uploads/docs/Mission_Booklets/AV/av_GPSIIF7_MOB.pdf

 Rocket/Payload: An Atlas V 401 will launch the GPS IIF-7 mission for the
 U.S. Air Force.

 Date/Site/Launch Time: Friday, Aug. 1, 2014, from Space Launch Complex
 (SLC)-41 at Cape Canaveral Air Force Station, Fla. The 18-minute launch
 window opens at 11:23 p.m. EDT.

 Viewing the Launch by Webcast: The live webcast will begin at 11:03 p.m.
 EDT.

 GPS IIF-7 is one of the next-generation GPS satellites, incorporating
 various improvements to provide greater accuracy, increased signals, and
 enhanced performance for users.

 Launch Updates: To keep up to speed with updates to the launch countdown,
 dial the ULA launch hotline at 1-877-852-4321 or join the conversation at
 www.facebook.com/ulalaunch and twitter.com/ulalaunch; hashtag #GPSIIF7.

 The Air Force Second Space Operations Squadron indicates that IIF-7,
 SVN-68/PRN-3, will replace SVN-43 in the F plane slot 3 (F3).  SVN-43 will
 be re-phased from F3 to the F2F slot to replace SVN-26.  SVN-33 will be
 taken out of the operational constellation the day after SVN-68 launch and
 sent to Launch, Anomaly and Disposal Operations (LADO).  SVN-33 was launched
 on 09 April 1996 successfully serving over 17.5 years, 10.5 years beyond its
 design life, due to the diligent efforts of the men and women of the U.S.
 Air Force. SVN-26 will back-up SVN-43 once it completes its re-phase
 journey.





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[time-nuts] R.I.N. Journals

2014-07-30 Thread Rob Kimberley
I have a box plus of Royal Institute of Navigation Journals going back
several years.

Free to a good home - UK  - collection only.

DE6 2AF post code.

Cheers

Rob Kimberley



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[time-nuts] Austron 1120 octal based oscillator

2014-07-30 Thread GandalfG8
I've recently acqured an octal based 4.096Mhz Austron  1120 oscillator that 
physically at least is a close match to the unit shown  in the data sheet 
on Didier's site.
 
However, this one, model 1120-1FWT dated 1981, which was indicated as  
being ex aircraft, looks to have significant connection differences.
Pins 2, 3, 5 and 7, for example, are all grounded to the case, whereas  the 
data sheet shows pins 2 and 3 as being respectively a 4V positive output 
and  the positive supply input.
Pin 1 has a consistent resistance of 4.6Kohm to ground and the  other pins 
all have resistances to ground of several megohms that show  variation if 
the meter polarity is reversed, suggesting the possibility of  capacitors 
across these.
 
From what little I've seen of other Austron oscillators they do seem  to 
have been quite consistent with their use of pin 3  as supply positive, which 
might not be good news, but I'll  assume for now that all is as it should be.
However, before I risk a bit of trial and error, has anybody else come  
across this or a similar variant or have any additional 1120 data that might be 
 relevant?
 
Regards
 
Nigel
GM8PZR
 
 
 
 
 
 
 
 
 
 
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Re: [time-nuts] Austron 1120 octal based oscillator

2014-07-30 Thread Bob Camp
Hi

Ok, so if it’s an 8 pin base you have:

1) unknown, 4.6 K to ground
2) ground
3) ground
4) unknown, cap?
5) ground
6) unknown, cap?
7) ground
8) unknown ,cap?

Next thing to check is pin 1 to 4,6,8. After that 4 to 6 and 8, finally 6 to 8. 

You *may* have a unit with a floating / isolated oven supply (say pins 6 and 8) 
and a grounded oscillator supply (say in on pin 4). The unit is certainly old 
enough to be from the split supply era.

Bob

On Jul 30, 2014, at 11:35 AM, gandal...@aol.com wrote:

 I've recently acqured an octal based 4.096Mhz Austron  1120 oscillator that 
 physically at least is a close match to the unit shown  in the data sheet 
 on Didier's site.
 
 However, this one, model 1120-1FWT dated 1981, which was indicated as  
 being ex aircraft, looks to have significant connection differences.
 Pins 2, 3, 5 and 7, for example, are all grounded to the case, whereas  the 
 data sheet shows pins 2 and 3 as being respectively a 4V positive output 
 and  the positive supply input.
 Pin 1 has a consistent resistance of 4.6Kohm to ground and the  other pins 
 all have resistances to ground of several megohms that show  variation if 
 the meter polarity is reversed, suggesting the possibility of  capacitors 
 across these.
 
 From what little I've seen of other Austron oscillators they do seem  to 
 have been quite consistent with their use of pin 3  as supply positive, which 
 might not be good news, but I'll  assume for now that all is as it should be.
 However, before I risk a bit of trial and error, has anybody else come  
 across this or a similar variant or have any additional 1120 data that might 
 be 
 relevant?
 
 Regards
 
 Nigel
 GM8PZR
 
 
 
 
 
 
 
 
 
 
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