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Michael Effinger

Researcher at Marshall Space Flight Center

Publications -  14
Citations -  838

Michael Effinger is an academic researcher from Marshall Space Flight Center. The author has contributed to research in topics: Solar wind & Primary mirror. The author has an hindex of 7, co-authored 12 publications receiving 675 citations.

Papers
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Journal ArticleDOI

Solar Wind Electrons Alphas and Protons (SWEAP) Investigation: Design of the Solar Wind and Coronal Plasma Instrument Suite for Solar Probe Plus

Justin C. Kasper, +80 more
TL;DR: The Solar Wind Electrons Alphas and Protons (SWEAP) Investigation on Solar Probe Plus is a four sensor instrument suite that provides complete measurements of the electrons and ionized helium and hydrogen that constitute the bulk of solar wind and coronal plasma.
Patent

Continuous fiber reinforced composites and methods, apparatuses, and compositions for making the same

TL;DR: In this article, a process for continuous composite coextrusion is described, which consists of forming a material-laden composition comprising a thermoplastic polymer and at least 40 volume % of a ceramic or metallic particulate in a manner such that the composition can be used as a substantially cylindrical feed rod, forming a hole down the symmetrical axis of the feed rod; inserting the start of a continuous spool of ceramic fiber, metal fiber or carbon fiber through the hole in the feed tube; extruding the feed rods and spool simultaneously to form a continuous filament consisting
Posted Content

The Habitable Exoplanet Observatory (HabEx) Mission Concept Study Interim Report

B. Scott Gaudi, +185 more
TL;DR: The Habitable Exoplanet Observatory, or HabEx, has been designed to be the Great Observatory of the 2030s, a space telescope with unique imaging and multi-object spectroscopic capabilities at wavelengths ranging from ultraviolet (UV) to near-IR.
Proceedings ArticleDOI

The development of stacked core technology for the fabrication of deep lightweight UV-quality space mirrors

TL;DR: In this article, the authors presented a proof-of-concept mirror for a 4m monolithic spaceflight UVOIR telescope with low areal density, thermally and dynamically stable primary mirrors.
Proceedings ArticleDOI

Cryogenic optical performance of a lightweighted mirror assembly for future space astronomical telescopes: correlating optical test results and thermal optical model

TL;DR: In this article, a 43cm diameter stacked core mirror demonstrator was interferometrically tested at room temperature down to 250 degrees Kelvin for thermal deformation, and the results of interferometric test, thermal IR images of the front face were recorded in order to validate thermal optical model.