Benefit Analysis of Hybrid CNT/CFRP Composites in Future Aircraft Structures

Period of Performance: 06/17/2015 - 12/17/2015


Phase 1 SBIR

Recipient Firm

Aurora Flight Sciences Corp.
9950 Wakeman Drive Array
Manassas, VA 20110
Firm POC
Principal Investigator


During Phase I, Aurora Flight Sciences and N12 Technologies propose to conduct a comprehensive analysis of the benefits of hybrid composites in future aircraft structures by leveraging analytical model and experimental results that Aurora has gathered during the development of its indigenous Orion unmanned aircraft system, which utilizes CFRP composites in the majority of its structure. Target areas that are critically loaded and/or include features such as embedded sensors and de-icing mechanisms, will be used to evaluate improvements in weight, lifecycle costs, performance, and reliability that CNTs can provide as a result of their multifunctionality. The analysis will be extended during Phase II to study the effect of hybrid composite utility on commercial aircraft (e.g. Boeing 737) using codes such as TASOPT that redesigns aircraft to optimize parameters including fuel efficiency and emissions. Phase II will also involve the design, build, and testing of hybrid composite specimens to prove out the benefits identified during Phase I. Relevant CNT data will be provided by N12 to ensure the greatest amount of accuracy in the benefit analysis. N12 is a spin-off from MIT Professor Brian Wardle's laboratory, that is capable of directly integrating vertically aligned CNTs with common aerospace-grade carbon prepreg materials and conventional processes used to manufacture primary aerospace structures (e.g. hand layup, automated fiber placement (AFP), automated tape layup (ATL)). N12 grows CNTs with controlled morphology and top-to-bottom alignment using an IP-protected continuous, high throughput process that is 1,000 times faster than common batch processes. These CNTs can similarly be transferred onto the surface of carbon prepreg materials in a continuous process that enables a seamless, low cost integration of CNT-reinforced CFRP prepreg with common manufacturing processes to enable future lightweight, multifunctional composite aircraft structures.