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Ham Satellite news

RS-12/13 tyst

Beacon frn RS-12/13 rapporterats har tystnat. Det finns ingen information om varfr detta skett.

Klla: ANS 1/9

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Ham Satellite news

AO-40 FAQ uppdaterad

AMSAT i USA har uppdaterat sin FAQ (frgor och svar) om Oscar 40. G in p deras hemsida och kolla.
http://www.amsat.org/amsat/sats/ao40/ao40-faq.html

Klla: AMSAT-NA

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Ham Satellite news

Senaste info 28 aug

Senaste info frn Oscar 40-teamet:

Because of the increasing ALON, it is now necessary to take pictures for attitude determination at the end of one orbit, and download them after apogee on the next orbit. This requires the IHU-2 to be left on through two passes of the radiation belts. Since EDAC is not currently active on the IHU-2, there is an excellent chance that it will crash about every second or third time this is done. A crash of the IHU-2 takes only a few minutes to correct, but until it is corrected the result will be an unmodulated tone on the middle beacon. If you should encounter this, be aware that the IHU-1 is running properly in the background and the command team will restore the beacon ASAP. The photos are not lost when the IHU-2 crashes, as long as the unit is not powered off.
The eclipses are continuing to lengthen and move later in the orbit. The timing of the beacon off interval will need frequent adjustment over the next several weeks. The interval will shortly be moved to MA 40 to 90.

–W4SM for the AO-40 Command Team

Klla: AMSAT-DL

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Ham Satellite news

Diskkrasch hos webmaster

Jag har ftt diskkrasch och kan drfr inte gra strre uppdateringar p AMSAT-SMs hemsida fr tillfllet.

Databasen, e-INFO och Oscar-40 nyheterna kan jag dock uppdatera via webgrnssnitt.

Hoppas komma igng under september!
73
Lars SM0TGU

Klla:

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Ham Satellite news

AMSAT-DL startar nya P-projekt

AMSAT-DL har nu krt igng tv nya satellitprojekt, P3-E och P5-A. Ls mer nedan:

AMSAT-DL announces formal go-ahead
for space missions
Phase 3-E and Phase 5-A

In July 2002 the AMSAT-DL (Germany) board of directors gave its official green light to develop and build the two spacecrafts AMSAT-Phase 3-E (P3E) and AMSAT-Phase 5-A (P5A). The high acceptance of the mission goals of these two projects expressed in the recent AMSAT-DL member s survey was the final element to arrive at this decision. Both satellites will be created in a common development process by an international team under the leadership of AMSAT-DL. The P3E satellite is to be launched as communication and scientific platform into a highly elliptical orbit around Earth. The second project with the working name AMSAT- Phase 5-A is destined to enter an orbit around the planet Mars. This spacecraft will then transmit scientific data to Earth – data from experiments on-board P5A as well as – via its repeater function – from experiments on the Martian surface or the planet s atmosphere.

So far three successful Phase 3 satellites were launched under the leadership of AMSAT-DL. The latest satellite of this series, P3D (now operational as AMSAT-OSCAR 40), was launched in 2000 and demonstrated sufficient bus and propulsion capabilities for a flight to Mars. So AMSAT-DL started a closer investigation into the possibility of such a mission. Based on the existing experience base and the overwhelming interest during the AMSAT-DL International Satellite-Workshop last year, the P5A spacecraft will not only carry scientific experiments, but also subpayloads to be released in direction to the Martian surface. Suitable launch windows to Mars exist in the years 2007 and 2009.

Two or three years earlier P3-E to be launched in an orbit around Earth is expected to continue the successful series of AMSAT- Phase 3 satellites. The main task of P3E is to serve as communication platform for the nearly 2 million radio amateurs worldwide. They constitute a network for further exploration of the so called uncoordinated multiple access , to provide simultaneous and freely available service to a large number of groundstations. Using existing technology and implementing the results of the member s survey, several transponders on frequencies between 145 MHz and 10 GHz are planned for P3E. Details will be fixed in a
design and payload meeting in the second half of 2002. Additionally the P3-E spacecraft will be an important test bed for some technology needed for the Mars mission. Work on the P3-bus has been started and a number of modules are already under construction.

So far all AMSAT-DL satellite missions in 1980, 83, 88 and 2000 were launched with ARIANE-launchers from French Guyana into geostationary transfer orbits. The excellent co-operation between Arianespace (with its current ARIANE-5-launch-system) and AMSAT-DL resulted in the development of various arrangements for the launch of secondary payloads on-board of ARIANE-launches. Thus Arianespace will be the first obvious choice for the launches of P3E and P5A.

Peter Glzow, DB2OS, President AMSAT-DL
Frank Sperber, DL6DBN, Vice President AMSAT-DL
Prof. Dr. Karl Meinzer, DJ4ZC, Projectleader

First background information about both missions can be found at:

http://www.amsat-dl.org/p3e/towards-p3e.pdf
http://www.amsat-dl.org/p5a/p5a-to-mars.pdf

Klla: AMSAT-DL

Categories
Ham Satellite news

Oscar 40 info juli

Nytt schema frn den 16 juli.
Information frn AMSAT-UK enligt nedan:

Effective this 765, on all days except Wednesday, the S2/K-Tx beacon only and passband segments are active again for testing. Note that the beacon only session (no passband) for S2 and K Tx s is MA 116-120, and the beacon + passband session is MA 120-128. As before, on Wednesday, the V-Rx along with L-band Rx s are connected to the passband from MA 120-128.

There s been some RUDAK issues too. Assi (I didn t know he was working on it) said:
The AO40 RUDAK team uploaded test code to one of the DSPs. This code generates a carrier at around 2401.625MHz ( doppler). The intent of this code is to help users do a ZR0 type experiment and test just how good their S-Band receive station is. The program generates a clean carrier at full RUDAK power, and then starts decreasing power in 3dB steps, all the way down to -30dB. One full cycle is 30 seconds. The resulting pattern is a sawtooth, and it is active between MA128 and MA160.

The code is new, and needs to be debugged. We would appreciate if some of you could record a wav file of the signal in SSB. If you can do so, please set your receiver so a clean tone is heard, and then record for at least 2 full minutes. During the recording don t update the frequency or mode so receiver phase modulation is not introduced. Once we get this code working, we will extend the period. If you can do this, please send Assi a zipped file emailed to 4x1kx@iarc.org

There were complaints about the amount of transmitter time RUDAK was taking; DB2OS commented:
The test code which Assi is working on is only a small part of things to come. This is to get a feeling about the I/Q modulator and performance of the DSP modems. And indeed it s a good test for you and other to test the system sensitivity, similar to the ZRO test in the good old days. The idea is to use the DSP modems for 1200 Bit/s BPSK PACSAT type operations, which would allow us to run RUDAK in parallel with the transponder passband.

Whatever will allow them to run the Passband and RUDAK downlink in parallel should be fine. 9600bps FM causes problems with distortion when the passband is on. 1200 Bit/s BPSK should be easy and if it works, they can look further ahead to other simultaneous digital modes.

Se ven ANS 202.

Klla: ANS 202, AMSAT-UK