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DTSTART:20170312T030000
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DTSTAMP:20170628T005128Z
UID:8EB31218-5AD7-11E7-8752-0050568D2FB3
DTSTART;TZID=US/Pacific:20170712T113000
DTEND;TZID=US/Pacific:20170712T130000
DESCRIPTION:IEEE Communications\, Signal Processing and Vehicular Technolog
 ies Joint Chapter invites you to a presentation by Dr. Siegfried Janson on
  the technology and challenges of designing a membrane spacecraft called 
 “Brane Craft” for active debris removal in low earth orbit. Flattening
  a spacecraft into a membrane can produce a low mass vehicle with an ultra
 -high power-to-weight ratio for rapid electric orbit transfers. The target
  application is removal of orbital debris in low Earth orbit (LEO) through
  rendezvous\, conformal wrapping\, and application of thrust.\n\nCo-sponso
 red by: The Aerospace Corporation\n\nSpeaker(s): Dr. Janson\, \, Dr. Janso
 n\, \n\nAgenda: \n11:20 am: Security in-processing and escort (for externa
 l guests)\n\n11:30 am: Networking\n\n12:00 pm: Presentation\n\n12:45 pm: Q
 &amp;A\n\n01:00 pm: Depart\n\nRoom: Atlas conference room 1029\, Bldg: A1\, 23
 10 East El Segundo Blvd\, El Segundo\, California\, United States\, 90245
LOCATION:Room: Atlas conference room 1029\, Bldg: A1\, 2310 East El Segundo
  Blvd\, El Segundo\, California\, United States\, 90245
ORGANIZER:clas.csv@gmail.com
SEQUENCE:5
SUMMARY:Brane Craft
URL;VALUE=URI:https://events.vtools.ieee.org/m/46063
X-ALT-DESC:Description: &lt;br /&gt;&lt;p&gt;&lt;span style=&quot;font-family: arial\, helvetic
 a\, sans-serif\; font-size: 12pt\;&quot;&gt;IEEE Communications\, Signal Processin
 g and Vehicular Technologies Joint Chapter invites you to a presentation b
 y Dr. Siegfried Janson on the technology and challenges of designing a mem
 brane spacecraft called &amp;ldquo\;Brane Craft&amp;rdquo\;&amp;nbsp\;for active debri
 s removal in low earth orbit.&amp;nbsp\;&amp;nbsp\;&amp;nbsp\;Flattening a spacecraft 
 into a membrane can produce a low mass vehicle with an ultra-high power-to
 -weight ratio for rapid electric orbit transfers.&amp;nbsp\; The target applic
 ation is removal of orbital debris in low Earth orbit (LEO) through rendez
 vous\, conformal wrapping\, and application of thrust. &lt;br /&gt;&lt;/span&gt;&lt;/p&gt;&lt;b
 r /&gt;&lt;br /&gt;Agenda: &lt;br /&gt;&lt;p&gt;&lt;span style=&quot;font-family: arial\, helvetica\, s
 ans-serif\; font-size: 10pt\;&quot;&gt;11:20 am: Security in-processing and escort
  (for external guests)&lt;br /&gt;&lt;/span&gt;&lt;/p&gt;\n&lt;p&gt;&lt;span style=&quot;font-family: aria
 l\, helvetica\, sans-serif\; font-size: 10pt\;&quot;&gt;11:30 am: Networking&lt;br /&gt;
 &lt;/span&gt;&lt;/p&gt;\n&lt;p&gt;&lt;span style=&quot;font-family: arial\, helvetica\, sans-serif\;
  font-size: 10pt\;&quot;&gt;12:00 pm: Presentation&lt;/span&gt;&lt;/p&gt;\n&lt;p&gt;&lt;span style=&quot;fon
 t-family: arial\, helvetica\, sans-serif\; font-size: 10pt\;&quot;&gt;12:45 pm: Q&amp;
 amp\;A&lt;/span&gt;&lt;/p&gt;\n&lt;p&gt;&lt;span style=&quot;font-family: arial\, helvetica\, sans-s
 erif\; font-size: 10pt\;&quot;&gt;01:00 pm: Depart&amp;nbsp\;&lt;/span&gt;&lt;/p&gt;\n&lt;p&gt;&amp;nbsp\;&lt;/
 p&gt;
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