Northrop Grumman Systems Corporation

Clinton Ung

Carl Baldwin Freidhoff

Sameh S Wanis

Vivian W Ryan

An apparatus for particle collection is provided. The apparatus includes a magnetic element configured to generate a tapered magnetic ion transport tunnel that collects particles from a local environment, a detector configured to perform one or more measurements of the collected particles, and ion optics configured to transport the collected particles to the detector.

Tapered magnetic ion transport tunnel for particle collection

An apparatus for radiation shielding is provided. The apparatus includes a first housing element and a first plurality of magnetic elements arranged in a first array on the first housing element. The first array is configured to generate a first tapered magnetic field and, using the first tapered magnetic field, deflect incoming radiation away from a protected element.

Radiation shield

A space ion analyzer in a spacecraft includes an axis and an aperture to receive an ion stream. An ion focuser to focus the ion stream along the axis responsive to a focus voltage, and an ion deflector deflects ions from the axis based on energies of the ions and a deflector voltage difference applied across plates of the ion deflector. A mass spectrometer on a chip (MSOC) directs ions from the ion deflector to an ion detector array responsive to an MSOC voltage difference applied to the MSOC. A focus voltage generator generates the focus voltage as a variable voltage referenced to a spacecraft ground. A deflector voltage generator generates the deflector voltage difference with a controllable magnitude and referenced to the spacecraft ground. An MSOC voltage generator generates the MSOC voltage difference with a controllable magnitude and referenced to a breaking potential controllable relative to the spacecraft ground.

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Ellicott City, MD, United States of America

Clinton Ung