NASA SBIR 2020-I Solicitation

Proposal Summary

 20-1- A1.10-5413
 Hypersonic/High Speed Technology - Seals and Thermal Barriers
 Improved Abrasion Resistance of High Temperature Seals
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Jackson Bond Enterprises, LLC
39 Industrial Park Road
Dover, NH 03820
(603) 742-2350

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)

Bruce Bond
39 Industrial Park Road Dover, NH 03820 - 4332
(603) 742-2350

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)

Justin Bond
39 Industrial Park Road Dover, NH 03820 - 4332
(603) 833-0805
Estimated Technology Readiness Level (TRL) :
Begin: 1
End: 4
Technical Abstract (Limit 2000 characters, approximately 200 words)

The development of new hypersonic (faster than Mach 5) vehicles is a high priority for the U.S., but the capabilities of existing sealing materials and components are stressed by the conditions of hypersonic flight.  Hypersonic vehicles require sealing materials between individual body panels and components of the weapons structure and propulsion system, including around dynamic flaps and rudders.  Current state-of-the-art high temperature thermal seals are often made from ceramic oxide fibers that are easily abraded at room temperature, even more so at sustained, elevated temperatures.  An abraded seal can lead to higher leak rates, increased temperatures, and decreased life-span (increased cost).  There is a need to improve the abrasion resistance of these seals without significantly reducing their other desirable characteristics (e.g., flexibility, temperature capability, flow-blocking).  To that end, Jackson Bond Enterprises LLC (JBE) proposes the following in Phase I.  First, JBE will partner with prime contractors and NASA stakeholders to research and identify potential abrasion resistant coatings and down-select the most promising coating types.  JBE has already identified two potential coating types in this proposal.  Second, JBE will manufacture coupons representative of high temperature seals and apply the chosen coatings.  Third, JBE will utilize in-house capability to perform abrasion testing on the coupons to determine the effectiveness of the coatings vs. baseline state-of-the art seals.  As a result of the work done in Phase I, one or more coatings will be identified, applied, tested for abrasion resistance, and either accepted or rejected for additional (Phase II) testing and development.

Potential NASA Applications (Limit 1500 characters, approximately 150 words)

Improved high-temperature seals would provide increased capability wherever seals are currently utilized such as reusable space vehicles and high-speed propulsion systems.  According to NASA’s HT Project website: “In the near-term, application of hypersonics research and technologies is likely to be on enhanced defense systems, but this could eventually expand to include improved access to space capabilities that would directly benefit NASA.” 

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words)

Near-term, the target market is DOD airbreathing hypersonic products such as the HAWC, TBG, CPS, and reusable ISR platforms and hypersonic delivery vehicles.  Long-term applications include commercial hypersonic aircraft that enable transcontinental flights for day long business trips.

Duration: 6

Form Generated on 06/29/2020 21:04:36