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Vertical Lift Air Vehicle Development

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Solicitation details, issuing organization, response deadlines, documents, and interested companies for this government contract opportunity.

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The Vertical Lift Air Vehicle Development subcontract supports the NASA Aeronautics Research Mission Directorate by providing specialized research for prime contractors. The scope of work focuses on advancing Urban Air Mobility safety, optimizing energy systems for vertical takeoff and landing, and developing innovative noise-reduction technologies for rotors and propellers. Technical execution involves the application of acoustic engineering, rotorcraft aerodynamics, and research into electric propulsion and battery systems. Key deliverables for this effort include the production of VTOL stability models, detailed acoustic profiles, and comprehensive safety analysis reports.

General Info

Subcontract for NASA research on VTOL safety, energy systems, and noise-reduction technologies.

Agency

National Aeronautics And Space Administration → Aeronautics Research Mission Directorate

NAICS

336413 - Other Aircraft Parts and Auxiliary Equipment Manufacturing

Place of Performance

Not specified

Set-Aside

NONE

Documents

This scope was carved out of NNH26ZEA001N.

The full solicitation package (1 document), including the RFP, is on the prime solicitation, not on this scope.

View the prime solicitation

RESEARCH OPPORTUNITIES IN AERONAUTICS (ROA- 2026)

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Timeline

PostedApr 27

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Organization & Contact Information

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AgencyNational Aeronautics And Space Administration → Aeronautics Research Mission Directorate

ContactsNo contacts available

OfficeN/A

Organization / AgencyNational Aeronautics And Space Administration → Aeronautics Research Mission Directorate

Office AddressN/A

ContactsNo contact information available

Full Description

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Performs research for prime contractors on NASA Aeronautics Research Mission Directorate projects. Develops noise-reduction technologies for rotors/props, researches Urban Air Mobility (UAM) safety, and optimizes vertical takeoff/landing (VTOL) energy systems. Employs rotorcraft aerodynamics, acoustic engineering, and battery/electric propulsion research. Delivers acoustic profiles, VTOL stability models, and safety analysis reports.

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Solicitation # NNH26ZEA001N

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