| Development of slow-burning solid rocket booster for RLV-TD hypersonic experiment A Parhi, V Mahesh, K Kalluru, S Reshmi, R Harikrishnan, VM Lakshmi, ... Current Science, 74-83, 2018 | 9 | 2018 |
| 3-D analysis of flanged joints through various preload methods using ANSYS J Paulmurugan, T Kurian, Jayaprakash, J, T Jayachandran, S Somanath Journal of The Institution of Engineers (India) : Series C 96, 407-417, 2015 | 7 | 2015 |
| Design and Thermo-Structural Analysis of the Interface between Subscale Versions of Carbon-Carbon (C-C) Nozzle Divergent to Metallic flange hardware for a Ground Simulation Test J Paul Murugan, T kurian 68th International Astronautical Congress (IAC-2017), Adelaide, Australlia, 2017 | 3 | 2017 |
| Effect of cooling medium on Solution treatment response of Titanium alloy Ti-5Al-5V-2Mo V Anil Kumar, RK Gupta, J Paul Murugan, J Srinath, SK Manwatkar, ... Materials Science Forum 830, 123-126, 2015 | 3 | 2015 |
| Design, development, static and flight tests of reverse flow multiple nozzle solid rocket motor with high burn rate propellant K Sreejith, S Prasad, R Bagavathiappan, C Prasanth, R Jeenu, ... Current Science, 116-121, 2021 | 1 | 2021 |
| Thermo-structural analysis of solid rocket scarfed nozzle with composite ablative liners for crew escape solid motor J Paul Murugan, T Kurian, G Levin, V Eswaran, J Jayaprakash, ... Advances in Astronautics Science and Technology 1 (1), 87-97, 2018 | 1 | 2018 |
| Structural assessment of Solid Rocket Motor hardware from the measured residual strain and 3-D profile in the long seam weld location J Paul Murugan, S Arora, T kurian, s Sivakumar 73rd International Astronautical Congress (IAC), International Astronautical …, 2022 | | 2022 |
| Thermo structural analysis and test results of solid rocket motor submerged Nozzle throat with 4-D Carbon-Carbon (C-C) and graphite material J Paul Murugan, T KURIAN, S SIVAKUMAR 73rd International Astronautical Congress (IAC), International Astronautical …, 2022 | | 2022 |
| A FLANGE JOINT ASSEMBLY T Paul Murugan,J IN Patent 382,674, 2020 | | 2020 |
| Thermo structural assessment of solid Rocket Motor Nozzle divergent assembly scheme flown in successful rocket mission J Paul Murugan, S Sivakumar, G Ayyappan ASET-2019 conducted by Aeronautical Society of India(AeSI), Oct 2019, 2019 | | 2019 |
| A Pseudo method for estimation of elastic plastic burst pressure of cylindrical pressure vessels and its experimental validation S kumar, J Paul Murugan, Y Arasu, T kurian International Astranautical Congress (IAC-2019), USA, Oct, 2019., 2019 | | 2019 |
| A configuration using retainer ring concept for connecting Motor case to Nozzle in a Solid Rocket Motor J Paul Murugan, R Thomas kurian,Bagavathiappan, ... IN Patent App. 2018 410 45,213, 2018 | | 2018 |
| Design Approach Adopted for Ensuring the Structural Integrity of Conduit Pipe Line Assembly Along the Solid Rocket Motor for an Air Breathing Technology Demonstration Flight J Paul Murugan, T kurian, J Jayaprakash, Rajarajan Journal of Aerospace sciences and technologies 70 (3A, August 2018 (Special …, 2018 | | 2018 |
| Thermo structural Analysis of Solid Rocket Scarfed Nozzle with composite Ablative Liners for Crew Escape Solid Motor A Paul Murugan,J: Thomas kurian, Rajarajan 69th International Astronautical Congress (IAC), Bremen, Germany, 1-5 …, 2018 | | 2018 |
| Numerical analysis of Igniter interface used in the first static testing of Low Altitude Crew Escape Solid Motor for the HSP pad abort flight’ J Swapnil kumar, Paul Murugan, T kurian 11th National conference and exhibition on aerospace and defense related …, 2018 | | 2018 |
| A study on the Design and Structural Analysis of Filament Wound Composite Motor case with Inter metallic Segment Joint J Paul Murugan, T kurian 68th International Astronautical Congress (IAC-2017), Adelaide, Australlia, 2017 | | 2017 |
| Un-symmetric Tang and clevis Joint J Paul Murugan, T kurian, R Bagavathiappan, J Jayaprakash IN Patent App. 2016 410 36,281, 2016 | | 2016 |
| Assessment of structural integrity of HPS3 Flex seal sub assembly to convergent sub assembly under reduced preload condition J Paul Murugan, T kurian 67th International Astronautical Congress (IAC-2016) , Guadalajara, Mexico …, 2016 | | 2016 |
| Design criticalities and structural integrity analysis of the spin-stabilization solid rocket motor charged with high energy grain" J Paul Murugan, S Arora, T kurian 67th International Astronautical Congress (IAC-2016), Guadalajara, Mexico …, 2016 | | 2016 |
| Structural analysis of a critical deviation observed at a interface in a Solid Rocket booster Motor using strain based criteria J Paul Murugan, T kurian 66th International Astronautical Congress (IAC-2015), Jerusalem, Israel, Oct …, 2015 | | 2015 |
Dr. Achutananda ParhiScientist/Engineer-‘SG’ , ISROVerified email at alumnimail.iitkgp.ac.in
Dr. Achutananda ParhiScientist/Engineer-‘SG’ , ISROVerified email at alumnimail.iitkgp.ac.in