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Towed Magnetic Anomaly Detection (MAD) Aerodynamic Modeling for Rotary Wing Platforms
Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-15-C-0265
Agency Tracking Number: N15A-009-0147
Amount:
$84,801.00
Phase:
Phase I
Program:
STTR
Solicitation Topic Code:
N15A-T009
Solicitation Number:
2015.1
Timeline
Solicitation Year:
2015
Award Year:
2015
Award Start Date (Proposal Award Date):
2015-06-15
Award End Date (Contract End Date):
2015-11-16
Small Business Information
PO Box 3426
Lawrence, KS
66046
United States
DUNS:
108339966
HUBZone Owned:
No
Woman Owned:
No
Socially and Economically Disadvantaged:
No
Principal Investigator
Name: Suman Saripalli
Phone: (785) 979-1116
Email: suman.saripalli@kalscott.com
Phone: (785) 979-1116
Email: suman.saripalli@kalscott.com
Business Contact
Name: Tom Sherwood
Title: Deputy Chief Technologist, AIR-4.5
Phone: (785) 979-1113
Email: tom.sherwood@kalscott.com
Title: Deputy Chief Technologist, AIR-4.5
Phone: (785) 979-1113
Email: tom.sherwood@kalscott.com
Research Institution
Name: University of Illinois
Contact: Michael Selig
Address:
Phone: (217) 244-5757
Type: Domestic Nonprofit Research Organization
Contact: Michael Selig
Address:
306 Talbot Laboratory, MC-236
104 S. Wright St
Urbana, IL
61801
United States
Phone: (217) 244-5757
Type: Domestic Nonprofit Research Organization
Abstract
The technical requirements for the simulation of a helicopter towing an aircraft while performing a MAD mission are identified. Several technical solutions to achieve high stability during the mission are presented. In Phase I, a simulation will be set up to begin trade studies on the proposed mission. Also, if needed, flight tests will be conducted in Phase I, as proof-of-concept validation. In Phase II, the designs will be refined and a spiral development of simulation and flight tests will be performed.
* Information listed above is at the time of submission. *
