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Pressurized Module
SPCF

Solution/Protein Crystal Growth Facility


Solution Crystallization Observation Facility (SCOF)

  The main purpose of using SCOF is to observe the crystallization process of many kinds of solutions. The observation includes interferometry, direct observation, photon-detection-counting and other methods and devices that support the accomplishment of many experiments. The experiment is performed using an automated program, which processes the experiment according to experiment parameters set in advance and installed in the program. In addition, tele-science operations are possible during the automated experiment by sending commands or parameter files to change or correct the experiment's performance.

SCOF features the following main components:

SCOF Main Components
SCOF Engineering Model

  The Main Section, which includes all components except the Experiment Cell Cartridge (Experiment Cell Section), consists of the following observation devices:

Mach-Zehnder Microscopic Interferometer

Michelson Microscopic Interferometer

Amplitude Modulation Microscope, Polarized Light Microscope, Bright-Field Microscope
 

The Experiment Cell Section is developed and prepared by each researcher based on the experiment requirements. In addition, each Experiment Cell Section can use these observation devices by utilizing the resources provided by SCOF Main Section
 

Observation Systems

The following diagram shows the observation mechanism of SCOF.

SCOF Observation System

(A) Mach-Zehnder Microscopic Interferometer

  The Mach-Zehnder Microscopic Interferometer can be used to observe the crystal growth using two different wavelengths that can be used to measure and analyze the temperature and concentration distribution of the solution in liquid-phase. The light path for the Mach-Zehnder Microscopic Interferometer follows the "vertical" axis so that passes through the Experiment Cell Cartridge from "top" to "bottom."
   

Magnification
x2 and x4
Light Source
Solid-state laser diode (l=532 nm and 780 nm)
Phase Difference Resolution
More than 0.2l
Spatial Resolution
More than 3.5 mm (for l=532 nm) and 5.0 mm (for l=780 nm)
CCD Image Sensor Size 1/2 inch


(B) Michelson Microscopic Interferometer 
The Michelson Microscopic Interferometer can also be used to measure the temperature and concentration distribution, with real-time phase-shift digital data. The light path for this interferometer follows the "horizontal" axis so that the side portion of the Experiment Cell Cartridge is observed.

Magnification x3
Light Source Solid-state laser diode (l=532 nm and 780 nm)
Phase Difference Resolution More than 0.02l
Spatial Resolution Less than 50 mm (for both l=532 nm and 780 nm)
CCD Image Sensor Size 1/2 inch (3CCD)


(C) Amplitude Modulation Microscope, Polarized Light Microscope, and Bright-Field Microscope
  The Amplitude Modulation Microscope, Polarized Light Microscope, and Bright-Field Microscope are available to observe the surface and morphology of the crystal. The light path for these microscopes follows the same optical axis as the Mach-Zehnder Microscopic Interferometer.

Magnification x2 and x4
Light Source Light Emitting Diode (LED, l=660 nm)
Phase Difference Resolution More than 1 mm
Spatial Resolution
More than 4.2 mm
Direction of Observation Transmitting or Reflective (Amplitude Modulation only)
CCD Image Sensor Size 1/2 inch


(D) Optional Observation and Measurement Devices
  In addition to the observation devices described above, the following devices may be added to enhance the facility's capabilities to facilitate experiments with a wide variety of observation targets.

Dynamic Light Scattering Measuring Device (DLS)

Fluorescent Decay Measuring Device

Reflection Spectrum Equipment (RSE)

Absorption Photometer

Other Devices
 
 
(1) Dynamic Light Scattering Measuring Device (DLS)

  In order to utilize the capability of Dynamic Light Scattering Measuring Device, the Experiment Cell Section needs to prepare a Photon Detector and optical fiber while Photon Counter and Hard Correlator Boards are already installed in the Main Section. The particle size distribution can be measured using a Hard-Correlator Method. The DLS has the following specifications: 

Light Source Solid-state Laser Diode (l=532 nm)
Particle Size Resolution Less than 10 nm
Particle Size Distribution Analysis Method Photon correlating method
 
(2) Fluorescent Decay Measuring Device
  This device shares the light source with DLS and a Photon-counter card is installed in the Electronic Controller (E-CONT) in the Main Section. The Experiment Cell Section needs to prepare a Band-path Filter that meets the electrical and mechanical interfaces supported by the Main Section.

(3) Reflection Spectrum Equipment (RSE)
 If the researcher requires Reflection Spectrum Equipment (RSE) for the experiment, SCOF Main Section provides physical and electrical interfaces for the Reflection Spectrum Equipment (RSE), including a RS232C Communication interface. The RSE itself needs to be developed by the Experiment Cell Section based on the interface and experiment requirements.

(4) Absorption Photometer
  If the researcher requires to use an Absorption Photometer, SCOF Main Section providesphysical and electrical mechanical, and optical interfaces to utilize the Absorption Photometer. Like RSE, the Absorption Photometer itself, including a halogen lamp and optical fiber, needs to be prepared by the Experiment Cell Section.

(5) Other Devices
  If an experiment requires a device that is not listed above, such device may be developed as part of the Experiment Cell Section, provided that the device meets the applicable interface requirements (mechanical, physical, electrical, and/or optical) with the Main Section.


 (E)Image data store and downlink capability
 Real-time image data can be stored in digital videotapes in IPU, and can be real-time downlinked through IPU in real time.

  In addition, the following components in the Main Section support the observation of the crystal growth:

Cell Driving System Provides mechanical interface with the Experiment Cell Section and allows the adjustment of optical positioning and focus.
Electronic Controller Regulates the components and communication including experiment data and commands.
Thermal and Fluid System Provides heat exhaustion out of SCOF with water coolant and avionics air. Also receives N2 gas for experimental purposes.
Operation Panel Provides interface with the flight crew. Also provides access to install and remove the Experiment Cell.


Interface Requirements between the Main Section and the Experiment Cell Section

  The interface requirements with the Main Section need to be met in order to develop the Experiment Cell Section for each experiment. The Main Section provides the following types of interfaces:

Physical Envelope

Mechanical Interface

Electrical Interface

Thermal Interface

Optical Interface

Fluid Interface

  These interfaces are controlled by the Interface Control Document (ICD) in which the English version will be available by middle of Year 2001. A brief description of these interfaces is shown in the following paragraphs. For details of these specifications, please refer to the ICD.

(A) Physical Envelope

  The principal envelope allowed for the Experiment Cell is 65 mm x 220 mm. However, an additional envelope of 300 mm x 120 mm x 240 mm may be utilized if any of the additional devices is required for the experiment.


(B) Mechanical Interface

  The mechanical mounting interface called Cell Stage is located on the Cell Driving System just inside of the door on the Operation Panel. Two pins and a mark are available to align the Experiment Cell and the Cell Stage. The Experiment Cell shall be fastened with screws attached to the Cell Stage.  An additional mechanical interface is available to attach the additional devices prepared by the researcher onto SCOF. This additional interface is located at the top rear of the Operation Panel. Unlike Cell Stage, only some holes are provided on a bracket such that the additional device may be attached using screws.
Moreover, if N2 gas is required for the experiment, the fluid shall be provided through a Quick Disconnect (QD), which serves as the mechanical interface.

(C) Electrical Interface

  SCOF Main Section provides power and signal lines to the Experiment Cell Section through six (6) connectors. The interface includes signals and power to thermistors, thermo-modules, heaters, thermocouples, pressure sensors, motors, and limit switches. In addition, data transmission through RS232C is available when using the RSE or other optional device. The following table shows the summary of these functions. For details, please refer to the ICD.
 

Control Device prepared by Cell Section Category Specification
Temperature Measurement Thermistor Ranges: Selectable from -10 to 220 degrees C, 10 to 80 degrees C, 15 to 65 degrees C, -1.5 to 0.5 degrees C, or 2.5 to 4.5 degrees C
Precision From +-2.60 degrees C to +-0.044 degrees C depending on the range selected.
Thermocouple Ranges: Selectable from -10 to 220 degrees C or -10 to 70 degrees C
Precision +-0.8% or +-1.6% corresponding to the range selected
Temperature Control Peltier Device - A maximum of 12 Peltier Devices can be used
Heater - A maximum of 2 heaters can be used.
Motor Control DC Motor - A maximum of 2 DC Motors can be used.
Stepping Motor - A maximum of 2 Stepping Motors can be used.
Pressure Measurement Pressure Sensor Ranges: Selectable from 0 to 69.03MPa (0 to 704 kgf/cm2), or 0 to 147.10MPa (0 to 1500kgf/cm2)
Position Detection Limit Switch - Mechanical Detection type.
Light Source LED Current 50mA Maximum.

  The electronic controller regulates all of these interfacing lines according to the experiment parameters preset into the software. Examples of the parameters include the timing to control the temperature to a target value, the selection of laser type, and selection of the observation device at different timing. Some of these parameters may be changed during the experiment by tele-science operation.
 

(D) Thermal Interface
  Most of the Experiment Cells are expected to utilize the heat exhaust capability of SCOF Main Section, as temperature control may play one of the critical roles for crystallization observation. Two main sources of heat exhaust are provided for the Experiment Cell: water coolant loop through a cooling block and avionics air flow within the SCOF Main Section. 
The cooling block is located underneath the Cell Stage thus heat exhaust is processed by metallic heat conduction through Cell Stage. The other source of heat exhaust, the avionics air flows from the sides of SCOF Main Section and to the rear section. The main purpose of the avionics air, however, is to cool down the rear of the Main Section; mostly the Electronic Controller. Approximately 120 W (maximum) of heat is may be released from the Experiment Cell.

(E) Optical Interface
  The optical interface is the most critical of all as the success of the experiment (observation) greatly depends on the optical design of the Experiment Cell. The following table shows the observation viewing range for each observation system and magnification:
 

Observation Device
Magnification
Observation Viewing Range
Mach-Zehnder Microscopic Interferometer Amplitude Modulation MicroscopePolarized Light Microscope
x2
2.4mm x 3.2mm
x4
1.2mm x 1.6mm
Michelson Microscopic Interferometer
x3
1.6mm x 2.1 mm

The Cell Driving System consists of motors that can be used to drive the Cell Stage (approximately }3.0 mm translation in three directions and }10 degrees rotation along the vertical (Z) axis) for optical adjustment of the Experiment Cell; mostly focusing and positioning.

(F) Fluid Interface
  If the experiment requires to substitute the gas or to create vacuum in the Experiment Cell during the experiment, SCOF Main Section can provide a N2 gas supply line and a gas release line to the Experiment Cell Section.

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Protein Crystallization Research Facility

  The main purpose of using PCRF is to generate high quality and large protein crystals by controlling the temperature of the specimen. Four crystallization methods are being employed on PCRF and all four methods can be processed simultaneously. Like SCOF, experiments on PCRF are performed using an automated program, which processes the experiment according to experiment parameters set in advance and installed in the program. Similarly, tele-science operations are possible during the automated experiment by sending commands or parameter files to change or correct the experiment's performance.

PCRF features the following main components:
 

PCRF Main Components
PCRF Engineering Model

Unlike SCOF, PCRF has only one observation system that consists of the following components:

CCD Camera

Optical Lens Assembly

Camera Movement Mechanism

PCRF Observation System

Image data store and downlink capability
 Real-time image data can be stored in digital videotapes in IPU, and can be real-time downlinked through IPU in real time.

 However, most of the other components that comprise PCRF are similar to those in SCOF:
 

Electronic Controller Regulates the components and communication including experiment data and commands
Thermal and Fluid System Provides heat exhaustion out of PCRF with water coolant and avionics air.
Operation Panel Provides interface with the flight crew. Also provides access to install and remove the Experiment Cell.

 

Interface Requirements between the Main Section and the Experiment Cell Section

  Like SCOF, the interface requirements with the PCRF Main Section need to be met in order to develop the Experiment Cell Section for each experiment. The Main Section provides the following types of interfaces:

Physical Envelope

Mechanical Interface

Electrical Interface

Thermal Interface

Optical Interface

  No fluid interface is provided for PCRF. However, like SCOF, these interfaces are controlled by the Interface Control Document (ICD) in which the English version will be available by middle of Year 2001(TBD). A brief description of these interfaces is given below:

(A) Physical Envelope
  The principal envelope for PCRF Experiment Cell Section is 100 mm x 150 mm x 65 mm (a schematic drawing to be placed later). On the drawing, six Cell Cartridges are shown and these dimensions account for one Cell Cartridge. However, one Experiment Cell Cartridge may utilize up to the envelope for two Cell Cartridges, if required by the experiment.

(B) Mechanical Interface
  The mounting interface for PCRF Experiment Cell Cartridge is the Cell Tray, which can accommodate up to six Experiment Cell Cartridges. Cell Tray provides two pins for alignment and two holes for fastening screws for each Experiment Cell Cartridge.

(C) Electrical Interface
  PCRF Main Section provides electrical lines for 2 thermistors, 1 thermomodule, 1 motor, and 1 photo-sensor for each Experiment Cell Cartridge. These electrical lines for one Cell Cartridge can be controlled independently of the lines for other Cell Cartridges. Therefore, temperature in each Cell Cartridge is controlled independently and will not be influenced by experiments simultaneously performed in other Cell Cartridges. This independent temperature control interface has the following specifications:
 

Number of channels
2 channels per Cell Cartridge Assembly
Temperature Measurement Range
0 to 35 degrees C
Precision of Measurement
+-0.5 degrees C

 
  Like SCOF, the electronic controller in PCRF Main Section regulates all interfacing lines according to the experiment parameters preset into the software. Examples of the parameters for PCRF include the timing to control the temperature to a target value, the duration of observation on one specimen, and the X-Y coordinates of the Cell (specimen) with respect to the camera for camera movement observation. Some of these parameters may be changed during the experiment by tele-science operation.

(D) Thermal Interface
  PCRF removes heat from the Experiment Cell Cartridges in a similar fashion as SCOF. A heat exchanging plate is located under the Cell Tray that conducts heat from the Experiment Cell Cartridges to the heat exchanger. Moreover, heat is removed also by avionics air which, like SCOF, flows from the side of PCRF and to the rear section. Approximately 120W of heat per 6 Cell Cartridge Assemblies can be removed through the Cell Tray.

(E) Optical Interface
The observation system in PCRF is has the following specifications:
 
Camera 1/2-inch CCD Camera
Light Source Light Emitting Diode(l=660nm)
Spatial Resolution More than 40 mm
  The camera can observe only one cell at a time but the camera can be moved to different positions at any time using commands or crew operations. (See the drawing)
 
Last update: November 21, 2003

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