Autonomous Satellite Docking System

Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: 99SB20113
Agency Tracking Number: 99SB20113
Amount: $94,657.00
Phase: Phase I
Program: SBIR
Awards Year: 1999
Solitcitation Year: N/A
Solitcitation Topic Code: N/A
Solitcitation Number: N/A
Small Business Information
MICHIGAN AEROSPACE CORP.
1050 Highland Drive, Suite E, Ann Arbor, MI, 48108
Duns: N/A
Hubzone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Michael Dobbs
 (734) 975-8777
Business Contact
Phone: () -
Research Institution
N/A
Abstract
Not Available The heating of high pressure sub-cooled liquid coupled with liquid-injected two-phase expansion is proposed as a pathway to a compact and high-efficiency combined cycle diesel engine. The concept is a novel and non-obvious departure from earlier industry efforts to develop high efficiency diesel engines. This new engine concept avoids the high temperature materials problems of prior high-efficiency engine concepts and has significant thermodynamic advantage over earlier combined diesel and Rankine cycle engines. The liquid injected expander eliminates the liquid-vapor phase separation requirement of conventional Rankine bottoming cycles and enables the miniaturization of system components. Also, the liquid injection cycle has a significant thermodynamic efficiency advantage over Rankine bottoming cycles in this combined cycle and enables the miniaturization of system components. Also, the liquid injection cycle has a significant thermodynamic efficiency advantage over Rankine bottoming cycles in this combined cycle application. This thermodynamic advantage stems from the ability to utilize the waste heat of the diesel engine over a wide temperature range. The combined diesel and liquid-injected expander engine concept allows for an economic breakthrough to a practical and highly efficient combined cycle diesel engine with a minimum of technical development. The economic feasibility of this new engine concept is an outgrowth of technology developments in compact heat exchanges, two-phase expanders, small high pressure pumps, and electronic controls. The power-to-weight ratio of the combined cycle engine should exceed that of conventional diesel engines.

* information listed above is at the time of submission.

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