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{
    "url": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/email/3TRPDDSWMOTRYEMA5GUSMOJAJFNVRT44/?format=api",
    "mailinglist": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/?format=api",
    "message_id": "[email protected]",
    "message_id_hash": "3TRPDDSWMOTRYEMA5GUSMOJAJFNVRT44",
    "thread": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/thread/3TRPDDSWMOTRYEMA5GUSMOJAJFNVRT44/?format=api",
    "sender": {
        "address": "wa6ilt (a) cox.net",
        "mailman_id": "e6a9df47e0344a0799fb4c07032df34a",
        "emails": "https://mailman.amsat.org/hyperkitty/api/sender/e6a9df47e0344a0799fb4c07032df34a/emails/?format=api"
    },
    "sender_name": "David Reinhart",
    "subject": "[AMSAT-BB] Battery chemistry",
    "date": "2020-12-10T10:34:28Z",
    "parent": null,
    "children": [],
    "votes": {
        "likes": 0,
        "dislikes": 0,
        "status": "neutral"
    },
    "content": "I can understand why we haven't been using lithium cells up until now, \nbut with the advent of LiFePO4 batteries is it possible they may be \nsuitable for satellite use? Or is the charging cycle unsuitable since it \nincludes temperature monitoring? I know on-orbit is different, but a \nlarge number of our local hams are now using these full-time to run \ntheir stations, continuously charged by AC or solar panels. In fact, our \nentire Field Day operation (should we ever get back into the field \nagain) is powered by a bank of these batteries; a 24v bus regulated down \nto 14 volts at each radio.\n\nDavid Reinhart, W4DSR\n\n",
    "attachments": []
}