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Shaver, Matthew David, author.
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intercept path. The entire lunar operational profile will be evaluated using nonlinear filter techniques
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Saranathan, Harish, author.
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trajectory is also significantly altered, which will in turn bear consequence on the design of the control
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Palmore, John Aaron, Jr., author.
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will have a few properties that make it suitable towards the goal of simulating vaporizing multiphase
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Kampmeier, Jennifer Lauren, author.
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show that the model is validated by altitude decay data from the MinXSS CubeSat, I will discuss areas
by
Stratton, Murphy C., author.
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this, the MSU 21 Meter Space Tracking Antenna will be used as a communications asset and to allow
by
Jude, Michael R., author.
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commercial efforts to mine asteroids. Such endeavors ultimately will require substantial amounts of
by
Gallaway, Scott, author.
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elements will cause changes to antenna gain and beamwidth. Under steady flight conditions this deflection
by
Ellery, Alexander, author.
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necessary for EVA-equivalence to afford maximum flexibility. Mutual collision possibilities will be
by
Tooth, Matthew Nathaniel, author.
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relatively underutilized methods that will prove valuable in future studies of changing predictor importance
by
Subedi, Hari B., author.
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infer the dynamic aberrations. In this work, we will present the working principle of the SAM wavefront
by
Abrantes, Richard Jun Espino, author.
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the model to any atomic species or any single application. This approach will enable researchers to
by
Hammerton, Jared Robert, author.
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actuators used to generate these wing geometries. Moving forward, the optimization will be applied over a