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Study of rarefaction effects in gas flows with particle approaches
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Atmosphere Occultation Student (ATOS) experiment
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The system architecting process for a solar power satellite concept
Arrhenius Reacting, One-Dimensional Flows With Equilibrium And Non-Equilibrium Initial Conditions
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Designing an optimal software intensive system acquisition: a game theoretic approach
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Reemployment Of Unemployed Scientists And Engineers From Aerospace Industries To Urban Government
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Theoretical and experimental investigtion into high current hollow cathode arc attachment
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Long term lunar radiation degradation of potential lunar habitat composite materials
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Incorporation of mission scenarios in deep space spacecraft design trades
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Spacecraft trajectory optimization: multiple-impulse to time-optimal finite-burn conversion
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Extravehicular activity (EVA) emergency aid for extended planetary surface missions: through-the-spacesuit intravenous (IV) administration
A study of ignition effects on thruster performance of a multi-electrode capillary discharge using visible emission spectroscopy diagnostics
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Experimental and numerical investigations of charging interactions of a dusty surface in space plasma
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Quantifying the effect of orbit altitude on mission cost for Earth observation satellites
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Performance analysis and flowfield characterization of secondary injection thrust vector control (SITVC) for a 2DCD nozzle
Characterization of space debris from collision events using ballistic coefficient estimation
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Stochastic peridynamics and upscaling
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A declarative design approach to modeling traditional and non-traditional space systems
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Advanced nuclear technologies for deep space exploration
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Development of impulse measurement techniques for the investigation of transient forces due to laser-induced ablation
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An analytical and experimental study of evolving 3D deformation fields using vision-based approaches
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Development and evaluation of high‐order methods in computational fluid dynamics
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Hydrogen peroxide vapor for small satellite propulsion
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Boundary layer and separation control on wings at low Reynolds numbers
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Return to the moon: MALEO, Module Assemby in Low Earth Orbit: A strategy for lunar base build-up
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