LMM Capability OverviewLMM Capability OverviewLMM Capability OverviewLMM Capability Overview Light...

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Gl R hC t Gl R hC t Glenn Research Center Glenn Research Center LMM Capability Overview LMM Capability Overview LMM Capability Overview LMM Capability Overview Light Microscopy Module Light Microscopy Module Fluids Integrated Rack Fluids Integrated Rack Fluids and Combustion Facility Fluids and Combustion Facility June 16, 2009 DeVon W. Griffin, Ph.D. NASA Glenn Research Center [email protected] (216) 433-8109 John T. Zoldak LMM Bio Capabilities – 1 ZIN Technologies [email protected] (440) 625-2334

Transcript of LMM Capability OverviewLMM Capability OverviewLMM Capability OverviewLMM Capability Overview Light...

Page 1: LMM Capability OverviewLMM Capability OverviewLMM Capability OverviewLMM Capability Overview Light Microscopy Module Fluids Integrated Rack Fluids and Combustion Facility June 16,

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LMM Capability OverviewLMM Capability OverviewLMM Capability OverviewLMM Capability Overview

Light Microscopy ModuleLight Microscopy ModuleFluids Integrated RackFluids Integrated Rack

Fluids and Combustion FacilityFluids and Combustion Facility

June 16, 2009DeVon W. Griffin, Ph.D.

NASA Glenn Research [email protected]

(216) 433-8109

John T. Zoldak

LMM Bio Capabilities – 1

ZIN [email protected]

(440) 625-2334

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Payloads in the Fluids Integrated RackGlenn Research CenterGlenn Research Center

Payload Specific Hardware FIR First Increment

The FCF FIR includes support subsystems and laboratory style diagnosticscommon to the specific researchers and supplements the laboratory withunique science hardware developed for each Payload.

Light Microscopy Module

Payload specific and multi-user hardwarecustomizes the FIR in a unique laboratoryconfiguration to perform research effectively.

Light Microscopy Module

Multi Use Payload Apparatus

FCF Fluids Integrated Rack• Power Supply• Avionics/Control

Common IlluminationPayload Specific Hardware• Sample Cell with universal Sample Tray• Specific Diagnostics• Specific Imaging• Fluid Containment

Multi-Use Payload Apparatus• Test Specific Module• Infrastructure that uniquely meets

the needs of PI experiments• Unique Diagnostics

S i li d I i

• Common Illumination• PI Integration Optics Bench• Imaging and Frame Capture• Diagnostics• Environmental Control

Data Processing/Storage

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• Fluid Containment • Specialized Imaging• Fluid Containment

• Data Processing/Storage• Light Containment• Active Rack Isolation System

(ARIS)

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The Light Microscopy ModuleGlenn Research CenterGlenn Research Center

Core Microscope Leica RXA adapted for spaceflight

Augmentation Automated operation and crew usable G d di Ground commanding

Capabilities---all in epi mode White light imaging White light imaging Fluorescence Köhler Illumination Linear illuminating wave plate

Camera Q-Imaging Retiga 1300

1280 x 1024; 1/3 inch CCD; 12 bits Binning: 1x1 to 4x4 Shutter: 0.0001 to 15 seconds

Location

LMM

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Fluids Integrated Rack, U.S. Module

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Current Hardware• Automated:

Possible Future Capabilities• Automated:

Objective turret, fluorescence turret and IC prism turret, field diaphragm, and aperture diaphragm

• Tube lenses: 1.0x, 1.25x, and 1.6x

• Polarization Analyzer (LMM)

• 3 Chip Color VGA Imaging (FIR)

• Nipkow disc confocal with 532 nm sample ( )

1.0x, 1.25x, and 1.6x

• Fluorescence cubes: DAPI, FITC, AND Chroma: red, blue, and green

• Epi Illumination Filters, singly or in combination: ND 0 4 1 6 436 nm and 546 nm

excitation (LMM)

• Bio flow chamber developed by TechShot

• Droplet immersion oil dispensed by an astronaut ND 0.4, 1.6, 436 nm, and 546 nm

• Stage Positioning: XY: 100 x 46; 2.5 micron resolution Z: 20 mm; 100 nm resolution

astronaut

• Trans-illumination XY stage with a condenser

• Automated imaging modes: Phase• Objectives:

0.5x (Bertrand Lens) 10x, N.A. 0.3 20x, N.A. 0.7, PH 2 40x N A 0 75

Automated imaging modes: Phase Contrast, DIC, Darkfield

• Dynamic Light Scattering

40x, N.A. 0.75 50x, N.A. 0.5, 7.1 mm working distance 63x, N.A. 0.7, PH 2 100x, N.A. 1.40, PH 3

• Containment for shatterable material

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Containment for shatterable material

• 236 GB image storage (FIR)

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Combined FIR / LMM CapabilitiesGlenn Research CenterGlenn Research Center

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Gl R h C tGl R h C tOil Immersion Objective Development

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• A sample holder supporting oil immersion objectives is inimmersion objectives is in development.

• The sample holder design t t ill i tisupports trans-illumination

using the existing stage.

• The sample holder will become pa resource for future users to utilize.

• The oil injection syringe can be• The oil injection syringe can be retrofitted to place biological samples on a test slide for direct measurement using andirect measurement using an immersion objective.

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BACKUP

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Th l h ld ll f• The sample holder allows for easy replacement of the sample cell by the ISS crew.

• The sample cell can be instrumented to measure temperature, pressure, etc

Sample Cell

• The sample cell can be filled on-orbit or on the ground prior to launch pending safetyto launch pending safety review.

• This design development is a i l l f th fl ibilitsimple example of the flexibility

available to support biological applications.

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Imaging 10X Darkfield100X Brightfield

Modes of the LMM

Microscope

S l 5 l tSample: 5 m polystyrene spheres in water.

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63X phase contrast 100X DIC