32 research outputs found
Testbed Validation of Location-Scheduled Control of a Reconfigurable Flux-Pinned Spacecraft Formation
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Architecting the Very-Large-Aperture Flux-Pinned Space Telescope: A Scalable, Modular Optical Array with High Agility and Passively Stable Orbital Dynamics
No full textFlux-Pinned Interfaces for the Assembly, Manipulation, and Reconfiguration of Modular Space Systems
No full textEffect of Composite Superconductor Structure on Dynamic Properties of Superconducting Interface and Formation in Space Application
No full textStrongly oxidizing perylene-3,4-dicarboximides for use in water oxidation photoelectrochemical cells
No full textPerylene-3,4-dicarboximide (PMI) based chromophores are explored for use in photoelectrochemical cells (PECs) for solar fuels generation.</p
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Design of a Fixed Wing Micro Aerial Vehicle
No full textThe goal of this project was to design, build, and fly a Micro Aerial Vehicle (MAV) to compete in the WPI MAV Competition. Points were awarded based on the aircraft’s largest dimension, flight time, ability to carry a payload, and perform onboard inertial measurements. Research was geared to design the smallest MAV while ensuring a four-minute flight time. An iterative design process was undertaken to arrive at the final MAV: a high-wing, fixed vertical tail aircraft, utilizing a Zimmerman wing planform with an area of 734 cm2 and a Selig 2027 airfoil, constructed out of polystyrene foam. The mass of the MAV was approximately 492 g. The MAV was powered by a lithium-polymer battery and Park 370 brushless motor and controlled by two elevons through a standard 2.4 GHz radio
Synthesis and transformations of metallocycles 5. Regioselective synthesis of ?-substituted alumocyclopentanes by the cyclometallation of ?-olefins using Et3Al in the presence of Cp2ZrCl2
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