NASA SBIR 2011 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 11-2 X10.01-8575
PHASE 1 CONTRACT NUMBER: NNX12CE83P
SUBTOPIC TITLE: Cryogenic Fluid Management Technologies
PROPOSAL TITLE: Reliable Actuator for Cryo Propellant Fluid Control

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Dynamic Structures and Materials, LLC
144 SE Parkway Court, Suite 160
Franklin, TN 37064 - 1307
(615) 595-6665

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Jeffrey Paine
jpaine@dynamic-structures.com
114 SE parkway Ct
Franklin, TN 37064 - 1307
(615) 595-6665 Extension :102

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 6

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Fluid handling applications in cryogenic and extreme environments require reliable actuation technology that can handle extreme temperatures, mechanical bind-up from ice and foreign contaminants, and operation in poor conditions. A novel EM hammer drive technology is proposed for use in cryo-propellant fuel storage and regulation valves/devices. In addition to high force, the new drive technology offers potential advantages for miniaturization, heat load reduction, and lower cost than traditional electromagnetic and piezoelectric actuators. Dynamic Structures and Materials (DSM) proposes to focus the Phase II innovation on the development of a hammer drive actuation mechanism that will take the EM oscillatory power and produce continuous linear motion for operation at cryogenic and extreme environments. DSM has demonstrated expertise in the operation of its high force linear motor actuators at temperatures down to 77 K. The proposed actuator should operate from approximately 4 K to 400 K and should provide very low or no out gassing as well as operational capabilities in hard vacuum. The technology is proposed for applications in the cryo fluid management, pressure and flow control, and driving operational equipment and instruments. This proposal addresses DSM's approach to the development of flight-scalable demonstration components for the EM hammer drive technology.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
DSM has received interest from NASA regarding actuators for cryogenic applications and for others that do not require low temperature capability. Many non-cryogenic uses require a wider temperature range than laboratory environment, so some of the proposed work would be useful for these purposes, as well. Many inquiries are related to the regulation of fluid flow or pressure. Thruster valves used in highly miniaturized satellites have received significant attention. Flow and pressure control of cryogenic propellants such as LOX for propulsion and LH2 is also an area of interest. As the technology is more fully developed, it will be practical to pursue applications requiring more force. Interest has been expressed in an actuator for a 1-inch and 2 inch cryo-isolation valve that will require over 150 pounds of output force. There are many cryo and non-cryo valve applications that can potentially be addressed by this technology.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The oil and gas transportation/handling/processing field is wide open for valve technology that can withstand extreme temperatures, high levels of contaminants, and provides intermittent operation in conditions that cause either temperature induced or contaminant induced binding. DSM's hammer-drive technology has a number of uses in this industry. DSM will look to specialists at oil industry research groups that will provide guidance for this market.
Applications outside NASA are other aerospace projects that require actuators to operate valves for cryogenic fluid handling. ESA and major US defense contractors have previously tested systems that used DSM's piezoelectric actuators. The US Air Force has expressed interest in very low temperature, high force actuators for use in their low Earth orbit simulation chambers at Arnold Engineering Development Center. More broadly, some commercial applications related to materials evaluation and inspection need positioning at very low temperature and could benefit from this research.

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.)
Actuators & Motors
Cryogenic/Fluid Systems
Deployment
Fuels/Propellants
Isolation/Protection/Shielding (Acoustic, Ballistic, Dust, Radiation, Thermal)
Microelectromechanical Systems (MEMS) and smaller


Form Generated on 09-03-12 17:04