| Studies on the role of iron oxide and copper chromite in solid propellant combustion K Ishitha, PA Ramakrishna Combustion and Flame 161 (10), 2717-2728, 2014 | 90 | 2014 |
| Sandwich propellant combustion: Modeling and experimental comparison PA Ramakrishna, PJ Paul, HS Mukunda Proceedings of the Combustion Institute 29 (2), 2963-2973, 2002 | 84 | 2002 |
| Effect of mechanical activation of high specific surface area aluminium with PTFE on composite solid propellant M Gaurav, PA Ramakrishna Combustion and Flame 166, 203-215, 2016 | 68 | 2016 |
| Towards the development of a high power density, high efficiency, micro power generator B Aravind, B Khandelwal, PA Ramakrishna, S Kumar Applied Energy 261, 114386, 2020 | 51 | 2020 |
| Studies on EVA‐Based Wax Fuel for Launch Vehicle Applications R Kumar, PA Ramakrishna Propellants, Explosives, Pyrotechnics 41 (2), 295-303, 2016 | 43 | 2016 |
| Innovative design to improve the power density of a solid oxide fuel cell PA Ramakrishna, S Yang, CH Sohn Journal of Power Sources 158 (1), 378-384, 2006 | 43 | 2006 |
| Effect of specific surface area of aluminum on composite solid propellant burning S Verma, PA Ramakrishna Journal of Propulsion and Power 29 (5), 1200-1206, 2013 | 41 | 2013 |
| Ageing studies on AP/HTPB based composites solid propellants H Naseem, J Yerra, H Murthy, PA Ramakrishna Energetic Materials Frontiers 2 (2), 111-124, 2021 | 39 | 2021 |
| Enhancement of hybrid fuel regression rate using a bluff body R Kumar, PA Ramakrishna Journal of Propulsion and Power 30 (4), 909-916, 2014 | 38 | 2014 |
| Measurement of regression rate in hybrid rocket using combustion chamber pressure R Kumar, PA Ramakrishna Acta Astronautica 103, 226-234, 2014 | 37 | 2014 |
| 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 | 35 | 2017 |
| Combustion of sandwich propellant at low pressures PA Ramakrishna, PJ Paul, HS Mukunda, CH Sohn Proceedings of the Combustion Institute 30 (2), 2097-2104, 2005 | 34 | 2005 |
| Issues Related to the Measurement of Regression Rate of Fast-Burning Hybrid Fuels R Kumar, PA Ramakrishna Journal of Propulsion and Power 29 (5), 1114-1121, 2013 | 33 | 2013 |
| Estimation of burning characteristics of AP/HTPB composite solid propellant using a sandwich model C Vijay, PA Ramakrishna Combustion and Flame 217, 321-330, 2020 | 32 | 2020 |
| Effect of protrusion on the enhancement of regression rate R Kumar, PA Ramakrishna Aerospace Science and Technology 39, 169-178, 2014 | 32 | 2014 |
| Dependence of density and burning rate of composite solid propellant on mixer size S Verma, PA Ramakrishna Acta Astronautica 93, 130-137, 2014 | 29 | 2014 |
| Activated charcoal–A novel burn rate enhancer of aluminized composite propellants S Verma, PA Ramakrishna Combustion and Flame 157 (6), 1202-1210, 2010 | 29 | 2010 |
| Investigations on activated charcoal, a burn-rate enhancer in composite solid propellant S Verma, PA Ramakrishna Journal of Propulsion and Power 29 (5), 1214-1219, 2013 | 23 | 2013 |
| Experimental investigation of temperature separation in a counter-flow vortex tube PA Ramakrishna, M Ramakrishna, R Manimaran Journal of heat transfer 136 (8), 082801, 2014 | 22 | 2014 |
| Activated charcoal: as burn rate modifier and its mechanism of action in non-metalized composite solid propellants K Ishitha, PA Ramakrishna International Journal of Advances in Engineering Sciences and Applied …, 2014 | 21 | 2014 |
Gaurav MarothiyaPhDVerified email at alumni.iitm.ac.in
