PLUG POWER INC

U435CFE FUEL CELL BACKUP POWER & ENERGY SECURITY

POWEREDGE R720, 125 EACH. LIMITED WARRANTY, RISERS, BROADCOM 5720, CHASSIS W/HARD DRIVE, RAID CONTROLLERS, INTEL XEON E5S. 8GB, 2000 EACH. 600GB HD, 1000 EACH. READY RAILS, SINGLE HOT-PLUG POWER SUPPLY AND POWER CORDS.

NASA LARC IS DEVELOPING A COMPACT, MULTI-WAVELENGTH HIGH SPECTRAL RESOLUTION LIDAR (HSRL) SYSTEM DESIGNED TO MEASURE VARIOUS OPTICAL AND MICROPHYSICAL PROPERTIES OF AEROSOLS AND CLOUDS. THE HSRL SYSTEM USES A HIGH POWER, PULSED, SEEDED ND:YAG LASER, WHOSE SEED IS WAVELENGTH-STABILIZED TO AN IODINE VAPOR ABSORPTION LINE. THE PRIMARY GOAL OF THE PHASE II EFFORT IS TO PROVIDE A ROBUST, NEXT GENERATION SEED LASER SYSTEM WHICH IS SIGNIFICANTLY REDUCED IN SIZE, WEIGHT, AND REQUIRED "WALL-PLUG" POWER FOR HSRL AND OTHER LIDAR APPLICATIONS. THIS APPROACH IS ENABLED BY USE OF A SUITABLE COMPACT LASER DIODE SOURCE, TOGETHER WITH ADVR'S INTEGRATED PLANAR LIGHTWAVE CIRCUIT (PLC) TECHNOLOGY. FURTHERMORE, ADVR'S MULTI-ELEMENT WAVEGUIDE TECHNOLOGY WILL BE UTILIZED IN THIS PHASE II EFFORT TO PROVIDE A COMPACT 355NM SOURCE, DERIVED FROM THE SAME SEED LASER, FOR CALIBRATION OF THE HSRL UV INTERFEROMETRIC FILTER. A COMPACT, NEXT GENERATION SEED LASER SYSTEM UTILIZING ADVR'S PLC AND UV TECHNOLOGY, INTEGRATED WITH A HIGH PERFORMANCE COMPACT LASER DIODE SOURCE WILL ADVANCE NASA'S LIDAR SYSTEMS DUE TO ITS COMPACT, EFFICIENT, AND RELIABLE DESIGN, THUS ENABLING USE ON SMALL AIRCRAFT AND SATELLITES.

U435CFE BAA-DEMO OF FUEL CELLS FOR BACKUP POWER

PLUG POWER SUPPLY

BACK UP FUEL CELL SYSTEM

GSA PASS-THROUGH LEASE FOR JFO

4512860235!CABLE, PLUG POWER X

QUANTUM OPUS IS EXCITED TO PROPOSE COMPACTIFYING, ENCLOSING, AND AUTOMATING ALL OF THE REQUIRED VACUUM, CRYOGENICS, AND ELECTRICAL SYSTEMS OF A SUPERCONDUCTING NANOWIRE SINGLE-PHOTON DETECTION SYSTEM INTO A 14-INCH TALL BY 17-INCH WIDE BY 18-INCH DEEP PACKAGE AND RE-ENGINEERING THE OPTICAL COLLECTION MECHANISMS TO BE COMPATIBLE WITH EXISTING NASA TELESCOPE INFRASTRUCTURE. THE END PRODUCT WILL BE A MULTI-OPTICAL-CHANNEL, RACK-MOUNTABLE SYSTEM ROUGHLY THE SIZE OF AN OSCILLOSCOPE WHICH CAN, AT THE PUSH OF A BUTTON, OR REMOTE COMMAND, GO FROM A COMPLETELY DORMANT TO ACTIVE STATE. THIS WOULD INCLUDE: PUMPING OUT ITS OWN VACUUM CAN, USING ACTIVE GETTERING TO INDEFINITELY PRESERVE VACUUM INTEGRITY, ACTIVATING THE INTEGRATED HELIUM COMPRESSOR AT APPROPRIATE VACUUM PRESSURE, AND BIASING THE NANOWIRE DETECTORS AT DESIRED BASE TEMPERATURE, WHILE ENABLING CONTINUOUS COUNTING FOR NEAR-INFRARED PHOTONS AT RATES APPROACHING 1 GHZ ON EACH OPTICAL CHANNEL. WALL PLUG POWER DRAW WILL BE≤300 W AND DOWN TIME FOR MAINTENANCE WILL ONLY BE REQUIRED EVERY 50,000 HOURS OF RUN TIME. THE SYSTEM WILL HOST TWO TYPES OF DETECTOR PAYLOADS, SINGLE-MODE FIBER COUPLED DETECTORS FOR INTEGRATION INTO TERRESTRIAL FIBER-OPTIC QUANTUM COMMUNICATIONS NETWORKS AND DETECTORS COUPLED TO 50-MICRON CORE GRADED-INDEX MULTIMODE FIBERS FOR CONNECTION TO TELESCOPES FOR EITHER CLASSICAL OR QUANTUM FREE-SPACE COMMUNICATION. DARK COUNT RATES ARE EXPECTED TO BE BETWEEN 1 AND 10 DARK COUNTS HZ PER 1550-NM MODE FOR A NET DARK RATE OF 1 TO 10 KHZ FOR THE MULTIMODE COUPLED DEVICES. THIS WILL BE A TRANSFORMATIONAL TECHNOLOGY ENABLING GLOBAL-SCALE DEPLOYMENT OF RECEIVER STATIONS FOR A SPACE-INTEGRATED, HYBRID CLASSICAL/QUANTUM, OPTICAL COMMUNICATIONS NETWORK FOR HIGH-RATE OPTICAL DATA RETURN FROM AND UNASSAILABLE SECURE COMMAND AND CONTROL COMMUNICATIONS TO SPACE TELESCOPES, ASTEROID MINING CRAFT, AND OTHER REMOTELY CONTROLLABLE SPACECRAFT.

AIRCRAFT PLUGS AND COVERS TO SUPPORT F-35 BEDDOWN ON MISAWA AB. - ENGINE INTAKE PLUG - POWER AND THERMAL MANAGEMENT SYSTEM PLUG - PITOT PROBE COVER W/ HEAT RESISTANT LINER - PMAC FLUSH PORT MODULE COVER (LEFT AND RIGHT) - A/C ENGINE EXHAUST PLUG