SBIR/STTR Research Award
Alternative Flight Control Methods for Supersonic/Hypersonic Cruise Missiles
Award amount
$69,849Program and phase
SBIR · Phase IAward year
2007Award details
- Awarding agency
- Department of Defense
- Branch
- Navy
- Recipient company
- KBM ENTERPRISES, INC
- Proposal award date
- 2007-05-04
- Contract end date
- 2008-02-04
- UEI
- MYQMZH69K4L3
- Solicitation number
- 2007.1
- Topic code
- N07-095
Research abstract
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.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- ACTUATOR INTEGRATED MISSILE STEERING SYSTEM (AIMSS) FOR SUPERSONIC MISSILES
- Alternative Flight Control Methods for Supersonic/Hypersonic Cruise Missiles
- ACTUATOR INTEGRATED MISSILE STEERING SYSTEM (AIMSS) FOR SUPERSONIC MISSILES