DEVELOPING A DESIGN OF A DUAL FLOW PATH NOZZLE FOR A TURBINE BASED COMBINED CYCLE PROPULSION SYSTEM.

Award details are derived from public USAspending.gov records. Not a bid recommendation.

Award details

Award ID: 80LARC25F7036
Contractor
Awarding agency: National Aeronautics and Space Administration
Sub-agency / office: National Aeronautics and Space Administration
Award amount: $1,248,634
Period of performance: Aug 27, 2025 – Nov 27, 2026
NAICS: 541715 — Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)
PSC: PSC AS22
Place of performance: OH
Parent award: 80LARC21D0002

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