Development of Turbopump Systems for Cryogenic and Semicryogenic Propulsion Systems of ISRO

Author:

Suresh M. S.ORCID

Publisher

Springer Science and Business Media LLC

Reference10 articles.

1. Abraham AM, Panigrahi S, Suresh MS (2017) Effect of pre-inducer in reducing net positive suction head requirement of a pump. J Propuls Power. https://doi.org/10.2514/1.B35514

2. Abraham AM, Unnikrishnan Nair P, Suresh MS (2020) Effect of blade configuration on performance of a high speed axial flow pump inducer. 71st IAC—The Cyber Space Edition

3. Choukekar KD, Nandi TK, George Paul P, Suresh MS (2009) Hydrostatic journal bearings for cryogenic rocket engine turbopumps: a review on the developments. Aerosp J Inst Eng (I) 90:3–8

4. Huzel DK, Huang DH (2002) Modern Engineering for design of Liquid-Propellant Rocket Engines. AIAA, Washington DC, pp 155–218

5. Kiran R, Sunil R, Harikumar K, Panigrahi S, Jayan N (2020) Effect of floating ring seal clearance on the performance of centrifugal pump used in liquid rocket engine. 71st IAC-The Cyber Space Edition

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