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ELIMINATION OF TURBULENCE-INDUCED STRUCTURAL FAILURE AND CONTROL LOSS IN VERY…

Award Information

Agency:
Department of Transportation 		Branch:
N/A 		Award ID:
1267 		Program Year/Program:
1985 / SBIR
Agency Tracking Number:
1267 		Solicitation Year:
N/A 		Solicitation Topic Code:
N/A 		Solicitation Number:
N/A
Small Business Information
Daedalus Research Inc.
P.O. Box 6067 Logan, UT 84341
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Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 1985
Title: ELIMINATION OF TURBULENCE-INDUCED STRUCTURAL FAILURE AND CONTROL LOSS IN VERY LIGHT AIRCRAFT
Agency: DOT
Contract: N/A
Award Amount: $300,000.00
 

Abstract:

A SYSTEM UTILIZING THE FREE-WING CONCEPT HAS BEEN DESIGNED FOR LIGHT AND VERY LIGHT WING-LOADING AIRCRAFT THAT ACCOMMODATES MODERATE TO HEAVY TURBULENCE WITHOUT TRANSMITTING HIGH GUST LOADINGS TO THE AIRFRAME OR THREATENING LOSS OF CONTROL. THE PROJECT WILL TEST THE SYSTEM IN A RESEARCH VEHICLE APPROXIMATING THE DESIGN CRITERIA SET FORTH IN 14 CFR, PART 103; THE RESEARCH VEHICLE IS UNMANNED.

Principal Investigator:

Richard Nelson
Scientist
0

Business Contact:

Small Business Information at Submission:

Daedalus Research, Inc.
108 N. Main Suite 208 Logan, UT 84321

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