Advanced Divert and Attitude Control (DACS) system for the Multiple (Miniature) Kill Vehicles (MKV)

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: HQ0006-06-C-7416
Agency Tracking Number: 053-0564
Amount: $99,990.00
Phase: Phase I
Program: SBIR
Awards Year: 2006
Solicitation Year: 2005
Solicitation Topic Code: MDA05-070
Solicitation Number: 2005.3
Small Business Information
1217 Smithfield Street, State College, PA, 16801
DUNS: 783589039
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: Y
Principal Investigator
 Kenneth Kuo
 Chief Scientist and President
 (814) 238-6989
 cpbt@mindspring.com
Business Contact
 Olivia Kuo
Title: Vice President
Phone: (814) 238-6989
Email: ojkuo@mindspring.com
Research Institution
N/A
Abstract
One possible method to intercept intercontinental ballistic missiles which deploy countermeasures is to use a "shotgun" approach, in which numerous small, cheap kill vehicles are deployed simultaneously in the hopes of scoring multiple hits. In order to be effective, such vehicles must be compact, inexpensive, reliable, and responsive. Miniaturizing a propulsion system is difficult because energetic materials may respond unpredictably at small scales in an intense combustion environment. We propose an innovative compact propulsion system, which will circumvent these concerns by using a liquid oxidizer as a coolant to prevent thermal effects from propagating through a pulse-operation-type motor. This system will utilize several self-contained gelled propellant charges. The oxidizing coolant will be injected into the motor from a bank of pre-pressurized tanks, maximizing the simplicity and manufacturability of the system; no pumps will be needed, and each propellant charge is modular and isolated from the others. The complete design will incorporate high energy density, high thrust, quick time response, high reliability, and relatively low expense. The probability of success for this project is high, since many energetic propellants have been developed by CPBT Corporation in previous SBIR studies. Commercialization of the new propulsion system has been planned for various applications.

* Information listed above is at the time of submission. *

Agency Micro-sites

SBA logo
Department of Agriculture logo
Department of Commerce logo
Department of Defense logo
Department of Education logo
Department of Energy logo
Department of Health and Human Services logo
Department of Homeland Security logo
Department of Transportation logo
Environmental Protection Agency logo
National Aeronautics and Space Administration logo
National Science Foundation logo
US Flag An Official Website of the United States Government