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{
    "url": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/email/PKF256QJFZGZOIJRJDVKYVKUDAMLQHNX/?format=api",
    "mailinglist": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/?format=api",
    "message_id": "[email protected]",
    "message_id_hash": "PKF256QJFZGZOIJRJDVKYVKUDAMLQHNX",
    "thread": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/thread/PKF256QJFZGZOIJRJDVKYVKUDAMLQHNX/?format=api",
    "sender": {
        "address": "bstrick (a) N5BRG.COM",
        "mailman_id": "953542c988dd4c549175bb02a8a6a1ed",
        "emails": "https://mailman.amsat.org/hyperkitty/api/sender/953542c988dd4c549175bb02a8a6a1ed/emails/?format=api"
    },
    "sender_name": "Bob Stricklin",
    "subject": "[pacsat] Power Thoughts",
    "date": "2022-10-28T15:19:09Z",
    "parent": null,
    "children": [],
    "votes": {
        "likes": 0,
        "dislikes": 0,
        "status": "neutral"
    },
    "content": "Group,\n\nPower requirments is something we need to be looking at carefully.\n\nI found this on the web:\n\nhttps://pressbooks-dev.oer.hawaii.edu/epet302/chapter/5-5-power-generation/\n\nWe can look at some data from other cubsats for power generation. Reviewing Falconsat-3 telemetry would be a good idea.\n\nPower and thermal design will play off each other.\n\nWith a 2.5 W power budget for a cubsat the pacsat payload could be a large power consumer. May effect ability to get onboard.\n\nIf Golf T had two of the TMS520 one must have been powered down until needed?\n\nDesigning for minimum power will yield more operating time and a longer mission life. Falconsat-3 is demonstrating this point now.\n\nBob N5BRG",
    "attachments": []
}