NASA SBIR 2015 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 15-1 Z1.01-9890
SUBTOPIC TITLE: Modeling and Measurements for Propulsion and Power
PROPOSAL TITLE: Electrospray Propulsion Engineering Toolkit (ESPET)

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Spectral Sciences, Inc.
4 Fourth Avenue
Burlington, MA 01803 - 3304
(781) 273-4770

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Rainer Dressler
rdressler@spectral.com
4 Fourth Avenue
Burlington, MA 01803 - 3304
(781) 273-4770

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Mrs. Leslie McCarthy
lmccarthy@spectral.com
4 Fourth Avenue
Burlington, MA 01803 - 3304
(781) 273-4770

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 2
End: 3

Technology Available (TAV) Subtopics
Modeling and Measurements for Propulsion and Power is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
To accelerate the development of scaled-up Electrospray Propulsion emitter array systems with practical thrust levels, Spectral Sciences, Inc. (SSI), in collaboration with Busek Co. Inc., proposes the development of an Electrospray Propulsion Engineering Toolkit (ESPET). The innovation is a multi-scale model that extends experimental and detailed high-level physics characterization of microfluidic components to full-scale ESP microfluidic network performance through an engineering tool with a central database of critical microfluidic properties. The tool is designed to allow ESP system engineers to efficiently narrow down the system component trade space and thereby substantially reduce the development time of advanced ESP systems. The physics underlying a microfluidic network of an ESP system covers multiple scale lengths that render the application of high-level CFD or atomistic molecular dynamics (MD) simulations over the entire system impractical. ESPET takes an engineering model approach that breaks the ESP system down into multiple microfluidic components or domains that can be described by analytical microfluidic solutions and specific parameters of the domain. The Phase I effort consists of a proof-of-principle of ESPET on the microfluidics of the Busek 100 micro Newton class ionic liquid ESP system. In Phase II, full development of ESPET for arbitrary designs will occur, including construction of the microfluidics properties database.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
For NASA to gain high-value science from SmallSat technology requires lightweight, miniaturized, precision impulse bit, fuel efficient propulsion systems that extend mission time and greatly enhance SmallSat utility. While a broad range of chemical and EP systems are under consideration for SmallSat thrusters, micro-fabricated electrospray (ESP) arrays have been clearly identified as an emerging technology for thruster attitude control as well as delta-v maneuvers, with scalability that also makes them attractive for applications on larger spacecraft. ESPET will accelerate the development of ESP systems that meet NASA requirements. ESPET will provide NASA with a tool for quick comparison of various fuels and thruster configurations. It will provide designers with estimates of thruster fuel and power efficiency, stability of output thrust, and potential for contamination effects. It will also enable them to develop accurate thruster control systems.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
SmallSat technology is bringing the space vehicle deployment cost within reach of a much larger market including small commercial enterprises like Cosmogia Inc.'s Dove-2 remote sensing mission for NOAA, research and educational initiatives like University of Florida's SwampSat demonstrator, and developing countries without a major space program, such as Poland's BRITE-PL for celestial observations. As the ESP technology becomes more generally available and new applications are envisioned, engineering software tools like ESPET will be essential to tailoring the thruster design to mission requirements. ESPET may also be extended to microfluidic system designs of miniaturized electrospray ionization sources for portable mass spectrometers.

TECHNOLOGY TAXONOMY MAPPING (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.)
Maneuvering/Stationkeeping/Attitude Control Devices
Models & Simulations (see also Testing & Evaluation)
Simulation & Modeling

Form Generated on 04-23-15 15:37