• I.Ganesh
• Dr.J.Santhosh

The aim of the project is to develop a urea bed neutralization method for neutralizing toxic rocket propellants in rocket engine test facilities. Di nitrogen tetraoxide and Monomethyl hydrazine are the hypergolic propellants used in rocket propulsion. These propellants are very toxic and high pollutant to the atmosphere. Rocket engines are to ground tested mandatory for performance evaluation. In rocket engines test facility propellants are stored in the propellant tank with high pressure. After engine testing, propellant has to be vented for safe test stand condition. But this propellant fumes polluting the environment. So neutralization of this fume of propellants is very essential for clean and safe environment. Hence a suitable neutralization method has to be developed with suitable agents and the output has to be analysed.

Ceramic balls. Monomethyl hydrazine, Neutralization, Nitrogen tetraoxide & Urea bed.

"EXPERIMENTAL ANALYSIS OF UREA BED METHOD FOR NEUTRALIZATION OF TOXIC ROCKET PROPELLANTS IN ROCKET ENGINE TEST FACILITIES", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.8, Issue 6, page no.a533-a536, June-2021, Available :http://www.jetir.org/papers/JETIR2106070.pdf

"EXPERIMENTAL ANALYSIS OF UREA BED METHOD FOR NEUTRALIZATION OF TOXIC ROCKET PROPELLANTS IN ROCKET ENGINE TEST FACILITIES", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.8, Issue 6, page no. ppa533-a536, June-2021, Available at : http://www.jetir.org/papers/JETIR2106070.pdf