USA flag logo/image

An Official Website of the United States Government

BOUNDARY LAYER PUMPED PROPULSION

Award Information

Agency:
National Aeronautics and Space Administration
Branch:
N/A
Award ID:
56622
Program Year/Program:
2003 / SBIR
Agency Tracking Number:
013581
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Advanced Propulsion Inc.
254 West Baseline Road, Suite 104 Tempe, AZ 85282 0126
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 2003
Title: BOUNDARY LAYER PUMPED PROPULSION
Agency: NASA
Contract: NAS1-02114
Award Amount: $600,000.00
 

Abstract:

Advanced Propulsion Inc. proposes a Revolutionary Concept (RevCon) integrated aircraft and propulsion system that provides aircraft drag reduction and propulsion system efficiency increase, thereby improving aircraft fuel efficiency by as much as a factor of two. The key feature is the ducting of a high fraction of the aircraft total boundary layer from distributed airframe inlets to turbofan engine(s) in the rear of the fuselage. This fully integrated, boundary layer pumping engine(s) will provide the sole propulsive thrust for the aircraft. API?s intent is twofold: First, to design the wing and fuselage configurations and boundary layer ingestion features for a very high fraction of laminar flow and greatly reduced parasitic drag. Second, to match the mass flow of the ingested boundary layer, the turbofan engine(s) and the aircraft cruise thrust requirement at the cruise design point to yield an extremely high level of propulsive efficiency. With reduced fuel loads, aircraft can be smaller, and less costly. With less drag and greater efficiency, aircraft can have higher performance. This integrated aircraft/propulsion technology is applicable to all types and sizes of subsonic airplanes.

Principal Investigator:

Gerald Merrill
Principal Investigator
4808291099
gmer1api@aol.com

Business Contact:

Gerald Merrill
Business Official
4808291099
gmer1api@aol.com
Small Business Information at Submission:

Advanced Propulsion Inc.
254 West Baseline Road, Suite 104 Tempe, AZ 85282

EIN/Tax ID: 860470529
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No