Optical Measurements of Rocket Nozzle Thrust and Noise
The high-temperature, high-speed exhaust from the propulsion systems of commercial systems, such as the SpaceX Falcon vehicles, impinges on the launch pad surface (see Space X, Merlin Engine in figure). This results in very high unsteady pressure loads and extremely high fluctuating thermal loads in the vicinity of the impingement region which leads to structural vibrations that can compromise efficiency and operational safety. The aeroacoustic loads due to rocket plume impingement and vehicle leading edge and boat-tail interactions will be experimentally examined in the research team's jet, rocket and aerodynamic facilities. The team will develop, test and refine promising Active, Passive and Hybrid flow control methods. Based on the results the team will identify the most promising method(s) in light of: flow unsteadiness reduction efficacy and full-scale implementation practicality.
- Record URL:
Language
- English
Project
- Status: Active
- Funding: $168935
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Sponsor Organizations:
Federal Aviation Administration Center of Excellence for Commercial Space Transportation
William J. Hughes Technical Center
Atlantic City International Airport, NJ United States 08405 -
Managing Organizations:
Federal Aviation Administration Center of Excellence for Commercial Space Transportation
William J. Hughes Technical Center
Atlantic City International Airport, NJ United States 08405 -
Project Managers:
Davidian, Ken
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Performing Organizations:
Florida State University
Tallahassee, FL United States 32901 -
Principal Investigators:
Kumar, Rajan
- Start Date: 20150903
- Expected Completion Date: 20180730
- Actual Completion Date: 0
Subject/Index Terms
- TRT Terms: Noise; Nozzles; Optical measurement; Spacecraft; Thrust
- Subject Areas: Aviation; Environment; Vehicles and Equipment;
Filing Info
- Accession Number: 01678246
- Record Type: Research project
- Source Agency: Federal Aviation Administration Center of Excellence for Commercial Space Transportation
- Files: RIP, USDOT
- Created Date: Aug 22 2018 1:03PM