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{
    "url": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/email/L7GAR5KQOIWF5M5HM6AR7IGBYQZGWQFR/",
    "mailinglist": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/",
    "message_id": "[email protected]",
    "message_id_hash": "L7GAR5KQOIWF5M5HM6AR7IGBYQZGWQFR",
    "thread": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/thread/DNIFMRNNSZ7S7QW6RV73AQ77G4NWPEMO/",
    "sender": {
        "address": "rwmcgwier (a) comcast.net",
        "mailman_id": null,
        "emails": null
    },
    "sender_name": "Robert McGwier",
    "subject": "[eagle] Re: Module Temperatures",
    "date": "2006-10-14T16:07:12Z",
    "parent": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/email/D7DWUURKWBDSFPR3Z65M2NLJOWM2NY5S/",
    "children": [],
    "votes": {
        "likes": 0,
        "dislikes": 0,
        "status": "neutral"
    },
    "content": "I think we should plan on sharing the antennas and we need to think \nabout the omni's for -Z eventually.  These are a lower priority than \nother tasks at the moment but they should be figured into the \"block \ndiagram\" in our minds.\n\n\nBob\n\n\n\nJim Sanford wrote:\n>\n> Will we share antennas or add some?\n> Jim\n>\n>\n> Robert McGwier wrote:\n>> I believe we should use Mirek's command receiver on L band as adapted \n>> for our purposes.  If we want a redundant one for any reason,  we do \n>> that one on 70cm.  The command receiver should feed the IHU-3 SDR for \n>> any normal commanding and any reset vector decoder we choose to enable.\n>>\n>> The issue is straightforward.   Any module that needs a heat sink will \n>> have been designed to be kept cool when the spacecraft is receiving a \n>> large thermal input from the sun.  When this thermal input is removed,  \n>> the same radiation cooling that was keeping the module cool will  \n>> continue to operate irrespective of the solar input.  That module will \n>> get cold over time.  If the bottom temperature stops the unit from \n>> operating properly and it is a command receiver,  this is not a good \n>> thing.   I believe we should have dedicated command receivers anyway and \n>> these to do not need 80 dB of dynamic range and can be made narrow \n>> band.  Our solar eclipse pattern has been given a preliminary analysis \n>> for the proposed orbit and we will be subjected to eclipses of \n>> insufficient duration to cause us severe thermal problems but what \n>> thermal issues there are need to be understood and this is what Dick is \n>> warning us about.  This analysis of the eclipse pattern was also the \n>> basis of my analysis that it would take well over a decade to subject \n>> any Li-ion battery to sufficient cycles to worry about.\n>>\n>> Bob\n>> N4HY\n>>\n>>\n>> John B. Stephensen wrote:\n>>   \n>>> The SAW filters work down to -35 C and the ICs to -40 C so its not too \n>>> far off. It's easy to use a lower power RF amplifier and mixer which \n>>> will lower the input intercept. Right now, the receiver is designed to \n>>> tolerate direct hits from PAVE PAWS at any two frequencies outside the \n>>> IF passband. As the input intecept is lowered, the percentage of \n>>> pulses that cause interference increases, but the receiver won't go \n>>> completely deaf as was reported on earlier satelites.\n>>>  \n>>> 73,\n>>>  \n>>> John\n>>> KD6OZH\n>>>\n>>>     ----- Original Message -----\n>>>     *From:* Dick Jansson-rr <mailto:[email protected]>\n>>>     *To:* AMSAT Eagle <mailto:[email protected]>\n>>>     *Sent:* Wednesday, October 11, 2006 17:51 UTC\n>>>     *Subject:* [eagle] Module Temperatures\n>>>\n>>>     Last evening I tried to convey the concept that the\n>>>     critical-command modules needed to be of low-power design to\n>>>     insure their operability during the occasional rather lengthy\n>>>     eclipse cooling of the spacecraft. My message apparently did not\n>>>     sink in. John reports that his design of such a U band receiver\n>>>     would be dissipating some 3.5W due to its bullet-proof nature\n>>>     against 3rd-order IM products needed for protection on the U band.\n>>>      \n>>>     If we go forward with such a module of that nature, it will need\n>>>     to have thermal control tapes on it to provide a mean emittance of\n>>>     about e=0.45. In a 3 hour eclipse we can expect to see spaceframe\n>>>     temperatures down to -100°C (173K) or lower. With such an\n>>>     environment John's module would be expected to see temperatures\n>>>     down to at least -44°C, which is a bit frosty for electronics that\n>>>     are expected to provide the critical services of commanding the\n>>>     spacecraft. Such operating temperatures are not felt to be\n>>>     advisable for that service.\n>>>      \n>>>     If John's module were of the 1W category, temperatures of the\n>>>     receiver could be expected to be in the range of -15°C to -20°C\n>>>     which would be more operable for the service.\n>>>      \n>>>     The above numbers are, of course, based on estimates which will be\n>>>     confirmed after we have the new spaceframe fully designed and\n>>>     analyzed. The \"warmer\" temperatures of the lower power modules are\n>>>     those that have been experienced and measured by telemetry from\n>>>     AO-10 and AO-13. These projections are thus based on 25 years of\n>>>     experience in these design concepts.\n>>>      \n>>>     /Dick Jansson/\n>>>     _---------------------------_\n>>>     [email protected] <mailto:[email protected]>\n>>>     _---------------------------_\n>>>\n>>>      \n>>>\n>>>     ------------------------------------------------------------------------\n>>>     _______________________________________________\n>>>     Via the Eagle mailing list courtesy of AMSAT-NA\n>>>     [email protected]\n>>>     http://amsat.org/mailman/listinfo/eagle\n>>>\n>>> ------------------------------------------------------------------------\n>>>\n>>> _______________________________________________\n>>> Via the Eagle mailing list courtesy of AMSAT-NA\n>>> [email protected]\n>>> http://amsat.org/mailman/listinfo/eagle\n>>>   \n>>>     \n>>\n>>\n>>   \n\n\n-- \nAMSAT Director and VP Engineering. Member: ARRL, AMSAT-DL,\nTAPR, Packrats, NJQRP, QRP ARCI, QCWA, FRC. ARRL SDR WG Chair\n\"You see, wire telegraph is a kind of a very, very long cat.\nYou pull his tail in New York and his head is meowing in Los\nAngeles. Do you understand this? And radio operates exactly\nthe same way: you send signals here, they receive them there.\nThe only difference is that there is no cat.\" - Einstein\n\n",
    "attachments": []
}