NASA SBIR 2008 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 08-2 S4.01-9107
PHASE 1 CONTRACT NUMBER: NNX09CC28P
SUBTOPIC TITLE: NanoSat Launch Vehicle Technologies
PROPOSAL TITLE: Thermal Control Nano-Sat

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Eclipse Energy Systems, Inc.
2345 Anvil Street North
St. Petersburg, FL 33710 - 3905
(813) 966-3627

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Kenneth Shannon
kshannon@eclipsethinfilms.com
2345 Anvil Street North
St. Petersburg, FL 33710 - 3905
(727) 344-7300

Expected Technology Readiness Level (TRL) upon completion of contract: 6 to 7

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Based on successful space testing onboard the Midstar1 satellite, Eclipse Electrochromics have been identified by a number of organizations as well as NASA as a high interest technology. For nanosats, the critical design challenge is achieving autonomous control of the EclipseVEDsTM for spacecraft thermal self regulation without the need for human intervention. To achieve this goal, Eclipse employed EclipseVEDTM technology and demonstrated the capacity to have automated control thermal systems capable of in-flight thermal regulation of a cubesat or other small satellite. In Phase II, Eclipse will build a complete multi-panel cubesat and work with NASA to lab test a completely functional prototype and review the capacity to utilize the ECDs concurrently with photovoltaics.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The electrochromic technology and its control systems suggested in the present proposal possess a wide range of applications relative to the needs of the Agency in satellite, spacecraft and component thermal control, space communications, chemical and biological monitoring of environmental control and life support systems, and in optical processing of information. The EclipseVEDTM developed by Eclipse Energy Systems, Inc. works as a voltage-controlled variable emissivity device to modify the thermal budget of satellites, spacecraft and space-based systems such as antenna networks, inflatable reflectors and habitable structures. The use of the technology with photovoltaics can also lead to longer missions, lower cost and more external area of the nano-sats used for other mission critical purposes.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Beyond the use as nanosat systems and the immense market for small space platforms for experiments in the commercial market, the EclipseVEDTM will be sold as an alternative to thermal control louvers prevalent in mid-size to large satellite systems comprising a $15M to $20M market. Typical louver systems add considerable mass to satellites (4kg/m2) in comparison to that associated with an IR ECD (15g/ m2). The use of EclipseVEDTM's to reduce thermal distortion in space-based antenna networks, reflectors, high altitude airships and habitable structures will reach a market estimated at $60M per annum. The EclipseVEDTM will find application in infrared beam steering for space-based communications, Fourier Transform Infrared (FTIR) spectrometers and infrared spatial light modulators for image processing. ECD and Photovoltaic combination can lead to household heating cost reductions.

NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.

TECHNOLOGY TAXONOMY MAPPING
Autonomous Reasoning/Artificial Intelligence
Ceramics
Computer System Architectures
Control Instrumentation
Cooling
Data Acquisition and End-to-End-Management
Data Input/Output Devices
Energy Storage
Highly-Reconfigurable
Metallics
On-Board Computing and Data Management
Optical & Photonic Materials
Photovoltaic Conversion
Reuseable
Semi-Conductors/Solid State Device Materials
Spaceport Infrastructure and Safety
Thermal Insulating Materials
Ultra-High Density/Low Power


Form Generated on 08-03-09 13:26