Low-Cost Autonomous Kinetic Energy (KE) Penetrator Payload for EX 172 Cargo Round

Award Information
Agency:
Department of Defense
Branch:
Navy
Amount:
$1,047,290.00
Award Year:
2005
Program:
SBIR
Phase:
Phase II
Contract:
N00178-05-C-1013
Agency Tracking Number:
N031-1550
Solicitation Year:
2003
Solicitation Topic Code:
N03-064
Solicitation Number:
2003.1
Small Business Information
TANNER RESEARCH, INC.
2650 East Foothill Boulevard, Pasadena, CA, 91107
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
195754056
Principal Investigator
 Amish Desai
 Scientist
 (626) 792-3000
 amish.desai@tanner.com
Business Contact
 Kevin Dinniene
Title: Controller
Phone: (626) 792-3000
Email: kevin.dinniene@tanner.com
Research Institution
N/A
Abstract
Tanner Research proposes to develop variable-sized thrusters packaged in digital-controlled arrays for high g applications in the ongoing development of exo-atmospheric hypervelocity projectiles (exo-HVP). Tanner’s multifunctional thruster concept is designed to be extensible for near-term use with gun-launched proof-of-concept prototypes, and the emerging EM gun-launched exo-HVP devices. The long-range exo-HVP must be reoriented at apogee into a nose-down attitude to achieve a smooth angle-of-attack for atmospheric reentry. A MEMS-based attitude control system (ACS) provides a low-cost methodology for embedding digital-controlled arrays of micro and macro-scale propulsion elements on an exo-HVP. MEMS fabricated devices have inherent gun-launch survivability at high g acceleration levels. Tanner’s thrusters were initially developed as a DACS for exo-atmospheric use with the miniature kill vehicle (MKV), a ballistic missile defense system (BMDS) concept implemented in hardware. Tanner’s digital-controlled micro thrusters are now being implemented in µUAV surfaces for maneuver control of endo-atmospheric applications, and other precision-guided autonomous munitions applications.

* information listed above is at the time of submission.

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