SBIR/STTR Research Award

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

Award identifier 9116599fb2e409c49c54e7fdc267860c90aae79d11d79a8fa421697ceba43050Awarding agency Department of Transportation

Award amount

$300,000

Program and phase

SBIR · Phase II

Award year

1985

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Award details

Awarding agency
Department of Transportation
Branch
Not reported
Recipient company
Daedalus Research Inc.
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research 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.

Technology keywords

Not reported

Agency intelligence

Department of Transportation

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