Aerodynamic Maneuvering and Control Actuation System for a Guided Destructive Expendable

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$750,000.00
Award Year:
2007
Program:
SBIR
Phase:
Phase II
Contract:
N68936-07-C-0054
Award Id:
77133
Agency Tracking Number:
N061-017-0328
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
4415 Euclid Avenue, Suite 500, Cleveland, OH, 44103
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
557510336
Principal Investigator:
Mehul Patel
Director, Aerodynamics Gr
(216) 649-0399
patel@orbitalresearch.com
Business Contact:
Joseph Snyder
Vice President
(216) 649-0399
snyder@orbitalresearch.com
Research Institute:
n/a
Abstract
Orbital Research Inc. (ORI) is investigating the use of a rocket-powered, guided destructive expendable (GuiDE) as a next-generation countermeasure for aircraft self-protection from missile attacks. The GuiDE is aimed to provide a low-cost alternative solution to existing airborne or ground-based aircraft countermeasure systems for protecting aircraft from beamriders and shoulder-fired anti-aircraft missiles such as man portable air defense systems (MANPADS). The system can also be integrated as a separate layer (Tier-2 or Tier-3) in a "layered" aircraft countermeasure system for enhanced coverage and padded protection. In this program, Orbital Research will design, build and test an Aerodynamic Maneuvering and Control Actuation System (AMCAS) on a candidate GuiDE airframe design compatible with the AN/ALE-50 Towed Decoy System. During the Phase I, ORI demonstrated the feasibility of multiple steering concepts in a low-speed wind tunnel, and examined the use of a GuiDE to counter hypothetical threat missiles approaching an aircraft from the rear hemisphere using six degree-of-freedom flight trajectory simulations. A study was also conducted to evaluate advanced seeker systems and the effect of seeker variables on the GuiDE design and control performance. During the Phase II, Orbital Research Inc. will advance the design and development of a candidate AMCAS and validate its performance on a candidate GuiDE design via experimental and modeling studies.

* information listed above is at the time of submission.

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