{"action":"created","issue":{"url":"https://api.github.com/repos/MatthewGrim/Lunar_SPS/issues/17","repository_url":"https://api.github.com/repos/MatthewGrim/Lunar_SPS","labels_url":"https://api.github.com/repos/MatthewGrim/Lunar_SPS/issues/17/labels{/name}","comments_url":"https://api.github.com/repos/MatthewGrim/Lunar_SPS/issues/17/comments","events_url":"https://api.github.com/repos/MatthewGrim/Lunar_SPS/issues/17/events","html_url":"https://github.com/MatthewGrim/Lunar_SPS/issues/17","id":339411047,"node_id":"MDU6SXNzdWUzMzk0MTEwNDc=","number":17,"title":"Equatorial Orbit - Constrained SPS Design 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issue is concerning the updates made to the constrained SPS design tool in order to accommodate the STK data report results of the equatorial SPS configuration."},"comment":{"url":"https://api.github.com/repos/MatthewGrim/Lunar_SPS/issues/comments/403841559","html_url":"https://github.com/MatthewGrim/Lunar_SPS/issues/17#issuecomment-403841559","issue_url":"https://api.github.com/repos/MatthewGrim/Lunar_SPS/issues/17","id":403841559,"node_id":"MDEyOklzc3VlQ29tbWVudDQwMzg0MTU1OQ==","user":{"login":"darianvp","id":38875772,"node_id":"MDQ6VXNlcjM4ODc1Nzcy","avatar_url":"https://avatars2.githubusercontent.com/u/38875772?v=4","gravatar_id":"","url":"https://api.github.com/users/darianvp","html_url":"https://github.com/darianvp","followers_url":"https://api.github.com/users/darianvp/followers","following_url":"https://api.github.com/users/darianvp/following{/other_user}","gists_url":"https://api.github.com/users/darianvp/gists{/gist_id}","starred_url":"https://api.github.com/users/darianvp/starred{/owner}{/repo}","subscriptions_url":"https://api.github.com/users/darianvp/subscriptions","organizations_url":"https://api.github.com/users/darianvp/orgs","repos_url":"https://api.github.com/users/darianvp/repos","events_url":"https://api.github.com/users/darianvp/events{/privacy}","received_events_url":"https://api.github.com/users/darianvp/received_events","type":"User","site_admin":false},"created_at":"2018-07-10T14:25:02Z","updated_at":"2018-07-10T14:25:02Z","author_association":"COLLABORATOR","body":"Due to the regular eclipsing of the SPS in an equatorial orbit, the utility of a battery for WPT is higher than in the case of the polar orbit (where the eclipsing is more irregular). Furthermore, the maximum event duration for which stored powered would be necessary in order to maintain the WPT link seems to be generally shorter than in the case of the polar orbit, meaning a smaller battery would be required. \r\n\r\nIn the case where only the pointing, power, and blackout requirements are applied for a SPS-Sorato link, a battery of 40 kg, charged fully for each stored power event, could reduce total blackout period by nearly 4% (an almost 50% increase in active time."}}
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