{"id":40,"date":"2016-12-19T20:20:59","date_gmt":"2016-12-19T20:20:59","guid":{"rendered":"http:\/\/m2i.aere.iastate.edu\/cysat\/?p=40"},"modified":"2016-12-19T20:20:59","modified_gmt":"2016-12-19T20:20:59","slug":"mission-analysis","status":"publish","type":"post","link":"https:\/\/m2i.aere.iastate.edu\/cysat\/2016\/12\/19\/mission-analysis\/","title":{"rendered":"Mission Analysis"},"content":{"rendered":"<h1>Mission Analysis<\/h1>\n<p>Mission Analysis is responsible for application of orbital mechanics to the practical problems concerning the motion the satellite. Additionally, the team is responsible for designing the mission architecture and assessing the feasibility of comprehensive mission designs. Mission Analysis is currently simulating potential Low Earth Orbits and will also be continuing research on Lunar and NEA simulations for the future.<\/p>\n<p>&nbsp;<\/p>\n<h2>Team Roster<\/h2>\n<table>\n<tbody>\n<tr>\n<td width=\"145\"><strong>Name<\/strong><\/td>\n<td width=\"108\"><strong>Year<\/strong><\/td>\n<td width=\"99\"><strong>Position<\/strong><\/td>\n<\/tr>\n<tr>\n<td width=\"145\"><strong>Jacob Goldenberg<\/strong><\/td>\n<td width=\"108\"><strong>Junior<\/strong><\/td>\n<td width=\"99\"><strong>Team Lead<\/strong><\/td>\n<\/tr>\n<tr>\n<td width=\"145\">James Wigda<\/td>\n<td width=\"108\">Senior<\/td>\n<td width=\"99\">Member<\/td>\n<\/tr>\n<tr>\n<td width=\"145\">Ross Wagener<\/td>\n<td width=\"108\">Freshman<\/td>\n<td width=\"99\">Member<\/td>\n<\/tr>\n<tr>\n<td width=\"145\">Nate Wernimont<\/td>\n<td width=\"108\">Junior<\/td>\n<td width=\"99\">Member<\/td>\n<\/tr>\n<tr>\n<td width=\"145\">Bryce Miles<\/td>\n<td width=\"108\">Freshman<\/td>\n<td width=\"99\">Member<\/td>\n<\/tr>\n<tr>\n<td width=\"145\">Christian Alvarado-Colon<\/td>\n<td width=\"108\">Senior<\/td>\n<td width=\"99\">Member<\/td>\n<\/tr>\n<tr>\n<td width=\"145\">Luke Gordon<\/td>\n<td width=\"108\">Sophomore<\/td>\n<td width=\"99\">Member<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<h2>Timeline and Milestones<\/h2>\n<p>&nbsp;<\/p>\n<table>\n<tbody>\n<tr>\n<td width=\"129\">Milestone<\/td>\n<td width=\"117\">Due Date<\/td>\n<td width=\"117\">Deliverable<\/td>\n<td width=\"117\">Points<\/td>\n<\/tr>\n<tr>\n<td width=\"129\"><strong>Mission Analysis CSLI Section Draft<\/strong><\/td>\n<td width=\"117\">September 29<sup>th<\/sup><\/td>\n<td width=\"117\">Written document including all Structures information for CSLI<\/td>\n<td width=\"117\">50<\/td>\n<\/tr>\n<tr>\n<td width=\"129\"><strong>Lunar STK Simulation<\/strong><\/td>\n<td width=\"117\">October 25<sup>th<\/sup><\/td>\n<td width=\"117\">Simulation in STK of a Lunar mission<\/td>\n<td width=\"117\">100<\/td>\n<\/tr>\n<tr>\n<td width=\"129\"><strong>Insert NEA into STK<\/strong><\/td>\n<td width=\"117\">November 30<sup>th<\/sup><\/td>\n<td width=\"117\">Find a way to insert a Near Earth Asteroid into STK<\/td>\n<td width=\"117\">50<\/td>\n<\/tr>\n<tr>\n<td width=\"129\"><strong>\u00a0<\/strong><\/td>\n<td width=\"117\"><strong>\u00a0<\/strong><\/td>\n<td width=\"117\"><strong>Total Points<\/strong><\/td>\n<td width=\"117\"><strong>200<\/strong><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<h2>Deliverables<\/h2>\n<p>&nbsp;<\/p>\n<h3>Mission ANalysis CSLI Section draft<\/h3>\n<p>The deliverable for Milestone 1 will be a draft document containing all Mission Analysis feasibility and merit report information, which will include degradation and access time estimates, optimal orbit characteristics, and figures of STK analysis.<\/p>\n<h3>Lunar STK Simulation<\/h3>\n<p>The deliverable for Milestone 2 will be a document showing the results from the Lunar missions simulation in STK, which will include life time and access time estimates.<\/p>\n<h3>INsert NEA into STK<\/h3>\n<p>The deliverable for Milestone 3 will be a document showcasing a NEA in STK and results from initial simulations.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Mission Analysis Mission Analysis is responsible for application of orbital mechanics to the practical problems concerning the motion the satellite. Additionally, the team is responsible for designing the mission architecture and assessing the feasibility of comprehensive mission designs. Mission Analysis is currently simulating potential Low Earth Orbits and will also be continuing research on Lunar<br \/><a class=\"moretag\" href=\"https:\/\/m2i.aere.iastate.edu\/cysat\/2016\/12\/19\/mission-analysis\/\">+ Read More<\/a><\/p>\n","protected":false},"author":1099,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[1],"tags":[],"class_list":["post-40","post","type-post","status-publish","format-standard","hentry","category-uncategorized"],"_links":{"self":[{"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/posts\/40","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/users\/1099"}],"replies":[{"embeddable":true,"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/comments?post=40"}],"version-history":[{"count":1,"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/posts\/40\/revisions"}],"predecessor-version":[{"id":41,"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/posts\/40\/revisions\/41"}],"wp:attachment":[{"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/media?parent=40"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/categories?post=40"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/m2i.aere.iastate.edu\/cysat\/wp-json\/wp\/v2\/tags?post=40"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}