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Astronomy & Space Sciences

Experimental and numerical investigation of the flame deflector for conditions ground testing of cluster nozzle stages

Implementing Organization

National Institute of Technology (Jalandhar), Punjab

Project Overview

The project aims to accurately predict and control the temperature load effect on flame deflectors with cluster rocket engine nozzle plume configuration in the real-time ground test facility. The noble design of the flame deflector is proposed to reduce the temperature load using water spray cooling with acoustic impact during real test conditions of the cluster rocket engine nozzle. Based on the operating conditions, empirical relations of heat transfer with steady and transient parameters of the deflector will be made, which suits the real-time applications.
Funding Organization
Funding Organization

Quick Information
Area of Research
Astronomy & Space Sciences
Focus Area
Aerospace Propulsion Testing
Status
Under Development
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
N/A
Startup (If Any)
00
No. of Patents
Filed :00
Grant :00
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