| Effect of mechanical activation of high specific surface area aluminium with PTFE on composite solid propellant G Marothiya, PA Ramakrishna Combustion and Flame 166, 203--215, 2016 | 68 | 2016 |
| An effective method to embed catalyst on AP and its effect on the burn rates of aluminized composite solid propellants G Marothiya, C Vijay, K Ishitha, PA Ramakrishna Combustion and Flame 182, 114-121, 2017 | 36 | 2017 |
| Effects on Burn Rates of Pellets and Propellants with Catalyst-Embedded AP G Marothiya, C Vijay, K Ishitha, PA Ramakrishna Journal of Propulsion and Power, 2018 | 11 | 2018 |
| Enhancement of aluminum reactivity to achieve high burn rate for an end burning rocket motor G Marothiya, PA Ramakrishna Propellants, Explosives, Pyrotechnics 42 (7), 816-825, 2017 | 8 | 2017 |
| Utilization of mechanically activated aluminum in hybrid rockets G Marothiya, PA Ramakrishna Journal of Propulsion and Power 34 (5), 1206-1213, 2018 | 7 | 2018 |
| Enhancement of Regression Rate in Hybrid Rockets G Marothiya, R Kumar, PA Ramakrishna 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2011 | 5 | 2011 |
| A New and Effective Method to Enhance the Burn Rate of Composite Solid Propellants G Marothiya, PA Ramakrishna 9th Asia-Pacific Conference on Combustion, 2013 | 4 | 2013 |
| Enhancing the regression rate of hydroxyl-terminated-polybutadiene-based mixed hybrid rockets G Marothiya, R Kumar, PA Ramakrishna Journal of Propulsion and Power 38 (4), 623-630, 2022 | 3 | 2022 |
| Enhancement of Regression Rate in HTPB Based Hybrid Rocket using Recrystallized AP and Pyral G Marothiya, PA Ramakrishna Ninth International Conference on Flow Dynamics, 252--253, 2012 | 3 | 2012 |
| Development of H2O2 Based Mixed Hybrid Rocket G Marothiya, PA Ramakrishna, N Saravanan, P Kumar Solasa Propellants, Explosives, Pyrotechnics 46 (11), 1687-1695, 2021 | 2 | 2021 |
| Coating Viton on Flake Aluminium and Its Effects on Performance of the Solid Rocket Motor G Marothiya, PA Ramakrishna 12th International Symposium on Special Topics in Chemical Propulsion …, 2021 | 2 | 2021 |
| Combustion of Flake Aluminum with PTFE in Solid and Hybrid Rockets G Marothiya, PA Ramakrishna Nano and Micro‐Scale Energetic Materials: Propellants and Explosives 1, 333-376, 2023 | 1 | 2023 |
| Development of H2O2 Based Hybrid Rocket for Sounding Rocket Application G Marothiya, PA Ramakrishna, N Saravanan, PK Solasa 12th International High Energy Materials Conference and Exhibits, 2019 | | 2019 |
| Role of Thermal Diffusivity in Determining Temperature Sensitivity V Chaitanya, G Marothiya, PA Ramakrishna 11th International High Energy Materials Conference and Exhibits, 2017 | | 2017 |
| Development of High Burn Rate Composite Propellant for Nozzleless Booster Application KG Sathesh, G Marothiya, PA Ramakrishna, J Sunitha Devi, ... 10th International High Energy Materials Conference & Exhibit, 2016 | | 2016 |
| Enhancement of Aluminium Reactivity to Achieve High Burn Rate for an End Burning Rocket Motor G Marothiya, PA Ramakrishna 10th International High Energy Materials Conference & Exhibit, 2016 | | 2016 |
| Experimental Validation and Study of a New High Performance Hybrid Propellant Combination M N. M, G Marothiya, PA Ramakrishna 2nd National Propulsion Conference, Mumbai, India, 2015 | | 2015 |
| A Novel Method to Obtain Temperature Sensitivity of Composite Solid Propellants G Marothiya, PA Ramakrishna 2nd National Propulsion Conference, Mumbai, India, 2015 | | 2015 |
| Enhancement of Regression Rate in Hybrid Rockets M Gaurav, K Rajiv, P Ramakrishna 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5911, 0 | | |
Ramakrishna PeriyapatnaDepartment of Aerosace Engineering IIT MadrasVerified email at iitm.ac.in
