SBIR-STTR Award

Alternative Flight Control Methods for Supersonic/Hypersonic Cruise Missiles
Award last edited on: 8/1/2007

Sponsored Program
SBIR
Awarding Agency
DOD : Navy
Total Award Amount
$69,849
Award Phase
1
Solicitation Topic Code
N07-095
Principal Investigator
Raymond A Deep

Company Information

KBM Enterprises Inc

PO Box 940
Ardmore, TN 38449
   (931) 468-9233
   kmsimmons@ardmore.net
   www.kbm-inc.com
Location: Multiple
Congr. District: 07
County: Giles

Phase I

Contract Number: N00014-07-M-0322
Start Date: 5/4/2007    Completed: 2/4/2008
Phase I year
2007
Phase I Amount
$69,849
The need to bring ordinance on `targets of opportunity' quickly before the target moves to another location is of paramount importance. A cruise missile that can travel at sustained hypersonic velocities could provide such a capability by reducing the time to target by a factor of 5 or more. Sustained flights at hypersonic velocities provide several technical challenges. Hypersonic control surfaces are typically thick, leading to high drag. High drag requires a high thrust power plant. Technology reducing drag will provide a very favorable trade to the overall missile system. KBM with GTRI propose a concept that utilizes actuators inserting small pins into the missile flow field to provide stability and control for a supersonic tailless missile. Inserting pins at the proper location can achieve high enough pressures on the body of a projectile or missile to produce high speed turns. Preliminary simplified simulation results have demonstrated that pins could be used to make a dynamically unstable tailless missile configuration fly a practically straight path.

Keywords:
Tailless, Finless, Supersonic, Hypersonic, Cruise Missile

Phase II

Contract Number: ----------
Start Date: 00/00/00    Completed: 00/00/00
Phase II year
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Phase II Amount
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