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Aerodynamic Design of a Dual-Flow Mach 7 Hypersonic Inlet System for a T...
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Development of a 10 Ah, Prismatic, Lithium-Ion Cell for NASA/Gsfc
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A Dual-Use Ballute for Entry and Descent During Planetary Missions
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Stirling Convertor Control for a Concept Rover at NASA Glenn Research Ce...
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Design, Fabrication, and Test of a Lox/Lch4 RCS Igniter at NASA
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A Computational Procedure for Identifying Bilinear Representations of Nonlinear Systems Using Volterra Kernels

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