SBIR/STTR Research Award

Advanced Aeroservoelstic Control for a Zero Emission Blended Wing Body Transport

Award identifier 14da690ff9fcc3c5e1865ecf08f6940531aec6bd7e0c3e0ff4c175c0c622837fAwarding agency National Aeronautics and Space Administration

Award amount

$149,960

Program and phase

SBIR · Phase I

Award year

2022

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
SYSTEMS TECHNOLOGY, INC
Proposal award date
2022-07-21
Contract end date
2023-01-25
UEI
R3DPJ1ZZJAK8
Solicitation number
SBIR_22_P1
Topic code
A1

Research abstract

It is a strategic thrust of the NASA ARMD to ldquo;realize revolutionary improvements in economics and environmenshy;tal performance for subsonic transports with opportunities to transition to alternative propulsion and energy.rdquo; To this end, JetZero Inc. has introduced the Ascent 2600, a novel zero emission blended wing body (BWB) commercial transport concept, to address this need. A key technology for this vehicle is an innovative landing gear concept, the pivot piston, that facilitates takeoff and landings without the need for high lift devices and enables entry into the single aisle transport market. In NASA SBIR Topic A1.01 a critical gap has been identified wherein ldquo;the use of lightweight flexible structures, the development of new airframes (truss-braced wings, blended-wing bodies, etc.), and the intentional exploitation of aeroelastic response phenomena require a comprehensive understanding of the aeroelasticity involved if they are to succeed.rdquo; This is certainly a recognized truth for the Ascent 2600 BWB, which will require innovative aeroelastic suppression methods to ensure desired ride qualities and safe operations for passengers that are no longer distributed along a relatively narrow tube. To this end a group of JetZero collaborators led by Systems Technology, Inc. (STI) propose the Active Control for Environmental disturbances and Structural interactions (ACES) system that will introduce novel active control techniques and will a feature a unique blend of the available wing, kink, and body control surfaces to mitigate undesirable aeroelastic interactions. Feasibility of ACES in Phase I will be demonstrated for the challenging gust load alleviation problem using the Ascent 2600 configuration, while in Phase II a broader range of aeroelastic problems including flutter suppression will be addressed with the effectiveness of ACES ultimately demonstrated in flight using the 13.5% dynamically scaled Pathfinder vehicle.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

187 SBIR/STTR records share this UEI (1983–2026). Reported award amounts total $58,450,871. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Health and Human Services, Department of Transportation, Department of Agriculture

Agency intelligence

National Aeronautics and Space Administration

Back to SBIR/STTR Research Awards

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