Mission length - PowerPoint PPT Presentation

1 Center for Detectors, Rochester Institute of Technology 2 MIT Lincoln Laboratory

A photon-counting detector for exoplanet missions Don Figer 1 , Joong Lee 1 , Brandon Hanold 1 , Brian Aull 2 , Jim Gregory 2 , Dan Schuette 2. 1 Center for Detectors, Rochester Institute of Technology 2 MIT Lincoln Laboratory. C f D. Detector Properties and SNR.

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475 views • 30 slides

Brian Erson Attitude Control Systems

Brian Erson Attitude Control Systems. Trans Lunar Phase Alternative Design Analysis Cold Xe Gas Thrusters. 1. Current H2O2 system. Advantages System is useful for an arbitrary payload mass No increased inert mass System has dual role in OTV and Lunar descent Disadvantages

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167 views • 5 slides

March 23B , 2010

March 23B , 2010 . Vertical structure, currents Eric the same path for sidescan and video Ulong pinchers Our vehicle ran at 15 meters across the channel and undulated Mission length = 8.615 km on the way back. Mission time = 1:47:37.

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94 views • 3 slides

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