Phase 1 of the program focused on developing and demonstrating a divert and attitude control system (DACS) that enables a kill vehicle to intercept hypersonic weapon threats during their glide phase.
Phase 2 will focus on quantifying aerodynamic jet interaction effects that result from DACS plumes and hypersonic air flows around an interceptor kill vehicle. The Glide Breaker Phase 2 Broad Agency Announcement (BAA) can be found at this link.
"Glide Breaker Phase 1 developed the propulsion technology necessary to achieve hit-to-kill against highly-maneuverable hypersonic threats. Phase 2 of the Glide Breaker program will develop the technical understanding of jet interactions necessary to enable design of propulsion control systems for a future operational glide-phase interceptor kill vehicle.
"Phases 1 and 2 together fill the technology gaps necessary for the U.S. to develop a robust defense against hypersonic threats," said Major Nathan Greiner, program manager in DARPA's Tactical Technology Office.
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