'Optical bench' diaporamas de présentation

2009 Olin Student Projects

2009 Olin Student Projects. Keith Gendreau Keith.c.gendreau@nasa.gov 301-286-6188 Phil Deines-Jones philip.v.deines-jones@nasa.gov 301-286-6884 Jeff Livas Jeffery.livas@nasa.gov 301-286-7289. 2009 Student Projects with contacts. Continuation of MCA Keith Gendreau

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FEMCI Workshop at GSFC 17 May 2001

FEMCI Workshop at GSFC 17 May 2001 STOP Analysis & Optimization of a very Low-Distortion Instrument HST WFC3 Case Study by Cengiz Kunt Swales Aerospace, Inc. HST. WFC3. OUTLINE.

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FEMCI Workshop at GSFC 17 May 2001

FEMCI Workshop at GSFC 17 May 2001 STOP Analysis & Optimization of a very Low-Distortion Instrument HST WFC3 Case Study by Cengiz Kunt Swales Aerospace, Inc. HST. WFC3. OUTLINE.

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charles.baker@nasa wschang@mscmail.gsfc.nasa

Lunar Reconnaissance Orbiter (LRO) Instrument Accommodations Review April 28, 2005 Thermal Design Charles Baker/GSFC Bill Chang/ESS. charles.baker@nasa.gov wschang@mscmail.gsfc.nasa.gov 301-286-2065 301-286-5703. Agenda. Status of Instrument Module Design

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ARIEL Atmospheric Remote-sensing Infrared Exoplanet Large survey

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HIRDLS SPARC Applications and Development Status

HIRDLS SPARC Applications and Development Status. John Gille University of Colorado and NCAR John Barnett Oxford University. Alyn Lambert, David Edwards, Christopher Palmer Michael Dials, Chris Halvorson, Eric Johnson, Wayne Rudolf Ken Stone, Bob Wells, John Whitney, Douglas Woodard.

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ISAS

ISAS. Astro-E. Hakucho (1979). Tenma (1983). to be launched on Feb. 8th, 2000. Ginga (1987). ASCA (1993). Institute of Space and Astronautical Science. 5.4 m. 6.5 m. Total Weight 1670 kg.

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ST7 Concept

The ST7 Interferometer Andreas Kuhnert Robert Spero Jet Propulsion Laboratory California Institute of Technology. ST7 Concept. Measure suspended masses within spacecraft Test thruster performance in drag-free control Hitch ride on LISA Pathfinder. x 1. x 2. Optical bench. TM1. TM2.

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Topics

Welcome to the laboratory specific Safety-Instruction for the laboratory course Measuring Techniques. Topics. Contact persons, laboratory personnel Requirements for the practical course Workflow of the practical course Protocols Safety instructions. Contact persons, laboratory personel.

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MAXIM Periscope Module

MAXIM Periscope Module. Structural Analysis Jeff Bolognese 25 April 2003. Structural Analysis Outline. Structural Analysis Goals Finite Element Models Analysis Results Issues and Future Work Conclusions Detailed Analysis Results Mirror Analyses Thermal Deformation

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Geostationary Operational Environmental Satellite R- Series GOES-R Overview and Status

Geostationary Operational Environmental Satellite R- Series GOES-R Overview and Status. Greg Mandt System Program Director 89 th AMS Annual Meeting January 13, 2009

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Interfaces of the Scientific Instrumentation, Telescope and Spacecraft

Interfaces of the Scientific Instrumentation, Telescope and Spacecraft. SKRIPUNOV EVGENY Lavochkin Association skrip @ laspace . ru. Presentation contents. Brief information about the T-170M Telescope Structural layout of the Scientific Instrumentation Complex Mechanical Interface

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Reflection of Light

Animations courtesy of Dr. Dan Russell, Kettering University. Reflection of Light. Reflection: the turning back of a wave after meeting the boundary of a medium. Types of Behaviors:. Scattered reflection. Regular Reflection. transmitted. absorbed.

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PALM3000 Realignment Winter 2007-2008

PALM3000 Realignment Winter 2007-2008. Jenny Roberts Optical Bench Team: C. Baranec, A. Bouchez, K. Bui, R. Burruss, R. Dekany, M. Troy Layout Design: A. Moore. Background.

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Radiation Damage Experience: SiPM & QIE Cards Proton Cyclotron - Mass General Hospital

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Chandra X-Ray Telescope

Chandra X-Ray Telescope. Abby Bradshaw Cole Butterfield. Expectations. Unprecedented x-ray images Spectra of violent, high temperature events Understand structure and organization of universe Detailed physics in a unique laboratory . Engineering .

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ASIM Instruments

ASIM Instruments. MXGS - Modular X-ray and Gamma-ray Sensor. MXGS consist of multiple units, structures and thermal systems. The sensor is made up of a Low Energy Detector (LED) and a High Energy Detector (HED).

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Paul McNamara on behalf of the LISA Pathfinder Science Working Team

Paul McNamara on behalf of the LISA Pathfinder Science Working Team.

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Sky visibility in 5 years from L2 Lagragian orbit

The World Space Observatory for UV (WSO/UV): implications for solar system studies. Isabella Pagano, Giuseppe Leto, Salvatore Scuderi, Giovanni Strazzulla INAF , Catania Astrophysical Observatory, Italy Noah Brosch

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