ARGOS Overview Angular Resolution at 2=550 nm: 5 arcsec Wavelength Regime 400-700 nm FOr (Field-of-Regard): 120(full cone)
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Introduction Objective: To compare the different imaging configurations for a Separated Spacecraft Interferometer operating from an Earths orbit
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Goal: Give necessary optics background to tackle a space mission, which includes an optical payload Light .Interaction of light w/environment o Optical design fundamentals Optical performance considerations .Telescope types and CCd design interferometer types
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Electromagnetic Formation Flight NRO DI Final review Friday, August 29, 2003 National reconnaissance office Headquarters Chantilly, VA LOCKHEED MART Massachusetts Institute of Lockheed Martin Corporation
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OVERVIEW OF THE EFFECTS OF THE SPACE ENVIRONMENT Outgassing in near vacuum Atmospheric drag Chemical reactions Plasma-induced charging Radiation damage of microcircuits, solar arrays, and sensors single event upsets in digital devices Hyper-velocity impacts
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Electrical Power System EPS Power Energy Power Power Regulation Source Storage Distribution and Control
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Outline Launch systems characteristics Launch systems selection process Spacecraft design envelope environments
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Earth Orbiting Clusters Edmund M C Kong SSL Graduate Research Assistant Prof david w. miller Director, MIT Space Systems Lab Space 2001 Conference& Exposition Albuquerque August28-30,2001
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