DARPA: Materials Architectures and Characterization for Hypersonics (MACH)

The  program aims to develop a new class of thermally-managed, shape-stable, sharp leading edge solutions for high lift-to-drag ratio hypersonic air vehicles that are capable of operating at high heat fluxes.

The MACH program will focus on:

(1) integrated leading edge thermal management solutions that are broadly applicable across different hypersonic configurations including boost-glide and air-breathing scramjet vehicles

(2) next-generation materials research for hypersonic vehicle leading edges.

 

 

Funding: No fixed limit 

Duration: 4 years 

 

Pls. check eligibility with PoC prior to submission. 

 

Research Authority due date: 4.11.19

Abstract (highly encouraged) due date: 11.2.19

Full proposal due date: 11.4.19