United States of America As Represented by the Administrator of Nasa

Manohar Deshpande

Charles Andrew Turner

Mark A Stephen

Fabrizio Gambini

Eleanya Onuma

Lawrence M Hilliard

An electromagnetic signal detector includes a photonic crystal substrate, an antenna disposed on the substrate and having an active feed region and a ground region spaced apart from one another by a gap, a photonic crystal disposed on the substrate at the gap, and an electro optic polymer disposed on the photonic crystal.

Integrated-photonic electromagnetic signal detector

A passive receiver system includes a first cross-dipole antenna on a platform, a second cross-dipole antenna on the platform, a passive receiver, and beam steering logic for the first and second cross-dipole antennas. The beam steering logic steers a radiation beam of the passive receiver in a first direction and steers the radiation beam of the passive receiver in a second direction. The first direction is aligned with a direct signal path and the second direction aligned with a reflect signal path. The platform is of a first satellite and the direct signal path is aligned with a second satellite.

Direction-of-arrival estimation for signal-of-opportunity receiver

A Cubesat uses both rail rods, walls, or both as an antenna. Either the rail rods and/or walls may form a rectangular waveguide, and may have one or more slots that allow energy to leak and radiate in a predefined direction in space.

Antenna for cubeSat platforms

An expandable and reconfigurable instrument node includes a feature detection means and a data processing portion in communication with the feature detection means, the data processing portion configured and disposed to process feature information. The instrument node further includes a phase locked loop (PLL) oscillator in communication with the data processing portion, the PLL oscillator configured and disposed to provide PLL information to the processing portion. The instrument node further includes a single tone transceiver and a pulse transceiver in communication with the PLL oscillator, the single tone transceiver configured and disposed to transmit or receive a single tone for phase correction of the PLL oscillator and the pulse transceiver configured and disposed to transmit and receive signals for phase correction of the PLL oscillator. The instrument node further includes a global positioning (GPA) receiver in communication with the processing portion, the GPS receiver configured and disposed to establish a global position of the instrument node.

Expandable and reconfigurable instrument node arrays

A step frequency inverse synthetic aperture radar (ISAR) includes a transmitter configured to transmit a transmission pulse at a transmission frequency to a near earth object (NEO), the transmission frequency having a frequency range comprising a starting frequency, an ending frequency, and a step size; a receiver configured to receive a pulse response from the NEO, the pulse response corresponding to the transmission pulse; and a computer configured to determine a 3-dimensional image of the interior of the NEO from the pulse response.

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Odenton, MD, United States of America

Manohar Deshpande