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{
    "url": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/email/ZO2AUNEZZ5BYZPAFPLWCNBHVZDRZ5WPM/",
    "mailinglist": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/",
    "message_id": "00f301c93bcf$7a0189c0$6a00a8c0@sparkys",
    "message_id_hash": "ZO2AUNEZZ5BYZPAFPLWCNBHVZDRZ5WPM",
    "thread": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/thread/ZO2AUNEZZ5BYZPAFPLWCNBHVZDRZ5WPM/",
    "sender": {
        "address": "sparkycivic (a) shaw.ca",
        "mailman_id": null,
        "emails": null
    },
    "sender_name": "Auke de Jong, VE6PWN",
    "subject": "[amsat-bb]  spaceflight(launch) question",
    "date": "2008-11-01T03:11:04Z",
    "parent": null,
    "children": [
        "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/email/R6QLHQ332QARUSDAKBGLD27FAKO6IGMT/"
    ],
    "votes": {
        "likes": 0,
        "dislikes": 0,
        "status": "neutral"
    },
    "content": "I was wondering... An question just occured to me that I couldn't answer: If a small satellite were hand-launched from the space station, and it contained an ion-drive motor powered by electricity, would it ever be able to accelerate in order to gain a higher orbit, or would that require an impracically large power supply/engine?  In other words, could that method be used to achieve higher orbits with communication/ham class satellites without having to use the typical large rocket we've been using all this time?  Also, would there be a cost-advantage to this method?\n\n\nAuke de Jong\nVE6PWN\nDO33go\nEdmonton, AB\n\n",
    "attachments": []
}