Xiomas Technologies
- View government funding actions
- Ypsilanti, MI 481978952
- Phone: 734-646-6535
- Corporate URL: www.xiomas.com
- Estimated Number of Employees: 3
- Estimated Annual Receipts: $530,000
- Business Start Date: 2007
- Contact Person: John Green
- Contact Phone: 734-646-6535
- Contact Email: johngreen@xiomas.com
- Business Structure:
- Partnership or Limited Liability Partnership
- Business Type:
- For Profit Organization
- Limited Liability f
- Industries Served: Engineering Services, Computer Systems Design Services, Research and Development in the Physical, Engineering, and Life Sciences (except Biotechnology)
- Product Areas: SUPPORT- ADMINISTRATIVE: TRANSLATION AND INTERPRETING, ADMIN SVCS/TRANSLATION-SIGN LANGUAG
Sampling of Federal Government Funding Actions/Set Asides
In order by amount of set aside monies.
- $66,334 - Sunday the 9th of December 2012
Forest Service
GEOSPATIAL SERVICE TECHNOLOGY CENTER
IGF::OT::IGF WIDE AREA IMAGER (WAI) SENSOR DEMONSTRATION/EVALUATION MISSION. PER ATTACHED PROPOSAL DATED 9/20/12. - $6,050 - Monday the 13th of February 2012
Department Of Navy
NAVAL RESEARCH LABORATORY
SOFTWARE - $124,992 - Friday the 10th of July 2015
National Aeronautics And Space Administration
NASA SHARED SERVICES CENTER
A HIGH PERFORMANCE, INEXPENSIVE, AIRBORNE SIMULATOR THAT WILL SERVE AS THE PROTOTYPE FOR A SMALL SATELLITE BASED IMAGING SYSTEM CAPABLE OF MAPPING THERMAL ANOMALIES ON THE SURFACE OF THE EARTH WITH A HIGH REVISIT RATE AND HIGH SPATIAL RESOLUTION IS PROPOSED. THE THERMAL MAPPING AIRBORNE SIMULATOR FOR SMALL SATELLITE SENSOR (TMAS) WILL BE DEVELOPED TO A TRL 8 IN THE PHASE II AND THE SPACE-QUALIFIED SYSTEM WILL BE DEVELOPED AND BUILT IN PHASE III. THE PROPOSED SYSTEM WILL DELIVER HIGH SPATIAL RESOLUTION (133 URAD), HIGH SIGNAL TO NOISE PERFORMANCE, TWO OR THREE SPECTRAL BANDS, AND ONBOARD PROCESSING TO EXTRACT THE INFORMATION OF GREATEST VALUE, ORTHORECTIFY THE IMAGERY, AND REDUCE THE SIZE OF THE DATA FOR TRANSMISSION. THIS SENSOR SYSTEM IS DESIGNED TO FIT WITHIN THE SIZE, WEIGHT, AND POWER (SWAP) ENVELOPES OF TYPICAL REMOTE SENSING AIRCRAFT AND SMALL SATELLITES. FOR THIS PROPOSAL WE HAVE DEVELOPED A NOTIONAL DESIGN THAT WILL BE REVIEWED AND FURTHER DEVELOPED DURING THE PHASE I. THE PROPOSED DESIGN INCORPORATES A STEP STARE SCANNING MIRROR, A TWO BAND (LWIR 8 TO 9 UM AND MWIR 4 5 UM) QUANTUM WELL INFRARED PHOTODETECTOR (QWIP), A SHORT WAVE IR SENSOR (1.6 UM), AND AN FPGA BASED IMAGE PROCESSING AND ORTHORECTIFICATION PROCESSING MODULE.
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