The Defense Systems Information Analysis Center (DSIAC) is seeking information on analyses or programs whose intent is to reduce effects that cause unstart in hypersonic airbreathing engines while maneuvering. This research is supporting a U.S. Department of Defense (DoD) organization looking for details on variable geometry design and/or shock/compression control for use on a multirange Mach number vehicle. Information on inlet/isolator design would also prove helpful.
If you have information that fits this request, please provide contact information, your title, and a short description either on this DoDTechipedia forum or in an email to Daniel Fleming, the DSIAC point of contact for this inquiry, or by clicking on the “Collaborate With Us” button below.