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{
    "url": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/email/TDVZ67OQPN5H26MN6FMT2U453SJ2HV6Z/",
    "mailinglist": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/",
    "message_id": "[email protected]",
    "message_id_hash": "TDVZ67OQPN5H26MN6FMT2U453SJ2HV6Z",
    "thread": "https://mailman.amsat.org/hyperkitty/api/list/[email protected]/thread/TDVZ67OQPN5H26MN6FMT2U453SJ2HV6Z/",
    "sender": {
        "address": "ku4os (a) cfl.rr.com",
        "mailman_id": null,
        "emails": null
    },
    "sender_name": "Lee McLamb",
    "subject": "[eagle]  Payload Adapters and excess launch margins",
    "date": "2007-07-19T02:31:22Z",
    "parent": null,
    "children": [],
    "votes": {
        "likes": 0,
        "dislikes": 0,
        "status": "neutral"
    },
    "content": "As Bob mentioned I attended the NASA/NRO Rideshare conference again this year.  \nI've just uploaded a file to Eaglepedia with one of the presentations which \nshows the current and some proposed secondary payload adapters presented by \nUnited Launch Aliance (ULA - the new Boeing & Lockheed-Martin partnership).  \nEspecially interesting is the 1000 and 1500 lb propellent margins for the \nAEHF and WGS missions on slide 11.  While we won't be ready for their first \nflight, both of these are the beginning of a constellation build-up which \nmeans there will be multiple re-flights for each.  Now I'm looking for an \nangle to get Eagle into an IPC for one of these missions.\n\nhttp://www.amsat.org/amsat-new/eagle/EaglePedia/uploads/a/aa/Keath_Karuntzoz_EELV_Secondary_Payload_Carriers_%28SPC%29.pdf\n\n73,\nLee-KU4OS\n",
    "attachments": []
}