Highly Compact Supersonic Cruise Missile (SSCM) Engine Inlet

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-12-C-0246
Agency Tracking Number: N121-028-0028
Amount: $79,833.00
Phase: Phase I
Program: SBIR
Awards Year: 2012
Solitcitation Year: 2012
Solitcitation Topic Code: N121-028
Solitcitation Number: 2012.1
Small Business Information
CFD Research Corporation
215 Wynn Dr., 5th Floor, Huntsville, AL, -
Duns: 185169620
Hubzone Owned: N
Woman Owned: Y
Socially and Economically Disadvantaged: N
Principal Investigator
 Mark Ostrander
 Group Leader
 (256) 726-4800
 proposals-contracts@cfdrc.com
Business Contact
 Deb Phipps
Title: Contracts Manager
Phone: (256) 726-4884
Email: dap@cfdrc.com
Research Institution
 Stub
Abstract
Future supersonic cruise missiles (SSCMs), such as the Next Generation Tomahawk, will require larger, more powerful engines to operate. Scaling current inlet technology to match will reduce missile body volume available for fuel, and hence curtail range. Highly compact inlet systems that allow efficient operation at supersonic speeds but are low-cost are needed to enable these missions. To be broadly-based, the SSCM inlet ducting must be initially folded and deploy after launch, so as to allow launch from either the VLS or torpedo tubes. CFDRC will design a scalable, deployable, compact supersonic inlet system that employs multiple ducts to minimize the interior inlet volume but that maintains efficient operation at all flight conditions. A low-cost external compression supersonic diffuser will be coupled with highly curved subsonic ducting to achieve this result. Deployment will be achieved by either hinging and folding, or pushing out the supersonic diffuser section. A strategy whereby both conventional S-duct and"innovative"minimum-volume concepts are explored will ensure program success. Initial configuration studies at design point will give way to more detailed optimization across the full flight spectrum in subsequent phases. CFDRC will work toward a Phase III goal of interfacing with engine and airframe companies such as Raytheon and Liberty Works to maximize participation in a Next Generation Tomahawk program.

* information listed above is at the time of submission.

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