NASA SBIR 2010 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 10-1 X2.01-9934
SUBTOPIC TITLE: Earth-to-Orbit Propulsion
PROPOSAL TITLE: Design Support and Analysis Tool for Pyrotechnically Actuated Valves

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Combustion Research and Flow Technology
6210 Keller's Church Road
Pipersville, PA 18947 - 1020
(215) 766-1520

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Ashvin Hosangadi
hosangad@craft-tech.com
6210 Keller's Church Rd.
Pipersville, PA 18947 - 1020
(215) 766-1520

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

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Pyrotechnically actuated valves are triggered on or off by firing an explosive charge that rapidly releases large amounts of high-pressure, gas. Pyrovalves are generally used for critical safety functions in almost all liquid and solid rocket systems and are designed to be fail-proof and provide extremely reliable actuation. However due to the lack of mature analysis tools, current design practices and safety analysis are heavily based on empiricism and are testing driven. The innovation proposed here is a comprehensive design and analysis tool that can characterize the transient performance of pyrotechnic actuators and provide a virtual test bed to assess performance and functional margin of these systems. The objective under this effort would be to develop a comprehensive three-dimensional transient tool that would simulate the gas –dynamic interactions with combustion, and model thermal effects in the valve material. For more complex initiator designs where multiple initiators may be fired, the tool could be used to identify "skew" effects resulting from the offset between the initiator firings. Since pyrovalves are ubiquitous and necessary for any rocket system, the tools and technology developed here would be useful to a broad variety of programs of core interest to NASA including the constellation program.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The end-product will be a high-fidelity, numerical simulation software (CRUNCH CFDREG code) that would predict the transient performance of pyrotechnic actuators, provide design support by supplementing current empirical rules, and diagnose system anomalies. Since pyrovalves are critical component of any space mission, our product addresses core needs of NASA missions including the Constellation program, the Mars science laboratory, as well as the new heavy lift rocket that may be designed. Pyrovalves are typically used for critical safety functions including emergency deployment of landing gears, chute deployment, and fuel flow control for thrusters. Consequently, pyrovalves have to be fail-proof and need to provide extremely reliable actuation with 99% reliability and 90% confidence interval level. However design and safety analyses have been largely testing driven and heavily based on empiricism since analysis and design tools are not mature. Our product addresses this critical need and would provide a reliable and well-validated tool.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The commercial market for our product is large and includes the broad aerospace and defense industry as well as safety and fire-suppression devices in the general industry including the nuclear, chemical processing and oil sectors. Pyrotechnic actuators are extensively used in products such as fire suppression systems (for deployment and dispersion of suppressants), electric disconnects in safety systems (for high speed termination of electrical circuits), air-bags and safety restraint systems (as a rapid gas generator), cable cutters and explosive bolts among numerous other applications. For these applications, characterizing the transient performance of the system is vital and the availability of a well-validated, reliable computational tool can play a key role in the design process for these critical elements. In addition to these traditional markets, commercial space ventures ranging from space transportation systems (COTS) for the international space station (ISS), to low-cost satellite launch systems would be receptive to this product.

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.)
Launch Engine/Booster
Maneuvering/Stationkeeping/Attitude Control Devices
Models & Simulations (see also Testing & Evaluation)
Software Tools (Analysis, Design)
Spacecraft Main Engine


Form Generated on 09-03-10 12:12