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Rajiv Kumar

Observed names: R. K. Kumar, R. Kumar
ORCID: 0000-0002-3108-6156
Observed ORCID: 0000-0002-3108-6156
OpenAlex ID: A5014730707
Supersonic combustion of hydrogen using an improved strut injection scheme
2019 · S. Aravind, Rajiv Kumar · International Journal of Hydrogen Energy · 88
Effect of multi-location swirl injection on the performance of hybrid rocket motor
2020 · Bala Vignesh, Rajiv Kumar · Acta Astronautica · 50
Studies on EVA‐Based Wax Fuel for Launch Vehicle Applications
2016 · Rajiv Kumar, Periyapatna A. Ramakrishna · Propellants Explosives Pyrotechnics · 46
Thermal decomposition and combustion studies of catalyzed AN/KDN based solid propellants
2016 · Pratim Kumar, Puran C. Joshi, et al. · Combustion and Flame · 43
Enhancement of Hybrid Fuel Regression Rate Using a Bluff Body
2014 · Rajiv Kumar, P. A. Ramakrishna · Journal of Propulsion and Power · 41
Issues Related to the Measurement of Regression Rate of Fast-Burning Hybrid Fuels
2013 · Rajiv Kumar, P. A. Ramakrishna · Journal of Propulsion and Power · 40
Development of EVA-SEBS based wax fuel for hybrid rocket applications
2018 · Dinesh Mengu, Rajiv Kumar · Acta Astronautica · 37
Effect of protrusion on the enhancement of regression rate
2014 · Rajiv Kumar, P.A. Ramakrishna · Aerospace Science and Technology · 35
Measurement of regression rate in hybrid rocket using combustion chamber pressure
2014 · Rajiv Kumar, P.A. Ramakrishna · Acta Astronautica · 32
Utility of Multiprotrusion as the Performance Enhancer in Hybrid Rocket Motor
2019 · Mengu Dinesh, Rajiv Kumar · Journal of Propulsion and Power · 30
The pressure effect study on the burning rate of ammonium nitrate-HTPB-based propellant with the influence catalysts
2011 · M. Pandey, S. Jha, et al. · Journal of Thermal Analysis and Calorimetry · 30
Protrusion effect on the performance of hybrid rocket with liquefying and non-liquefying fuels
2020 · Mengu Dinesh, Saideep Singh Rajput, et al. · Acta Astronautica · 25
Effect of Protrusion in the Enhancement of Regression Rate in Hybrid Rocket
2011 · Rajiv Kumar, P. Ramakrishna · AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC) · 14
Catalytic effects of Cu-Co* on the thermal decomposition of AN and AN/KDN based green oxidizer and propellant samples
2018 · Pratim Kumar, Puran Chandra Joshi, et al. · Defence Technology · 13
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Experimental Studies of Protrusion-Inserted Hybrid Rocket Motor with Varying L/D Ratio
2020 · Mengu Dinesh, Rajiv Kumar · Journal of Spacecraft and Rockets · 12
Simulation and Experimental Study of Torque Vectoring on Vehicle Handling and Stability
2009 · Rajiv Kumar, Bharath K Suda, et al. · SAE technical papers on CD-ROM/SAE technical paper series · 9
Evaluation of combustion stability of single and multi-protrusion inserted hybrid rocket motor
2024 · Dinesh Mengu, Rajiv Kumar · Acta Astronautica · 7
Effect on the performance of a hybrid rocket using AP in the PVC and HTPB-based hybrid fuel
2024 · Mehdi Abbas, Rajiv Kumar, et al. · FirePhysChem · 6
Experimental studies on swirl injector with varying L/D ratio of hybrid rocket motor
2024 · Arpit Dubey, Rajiv Kumar, et al. · International Journal of Heat and Fluid Flow · 4
Enhancing the Regression Rate of Hydroxyl-Terminated-Polybutadiene-Based Mixed Hybrid Rockets
2022 · Gaurav Marothiya, Rajiv Kumar, et al. · Journal of Propulsion and Power · 4
Thermal Decomposition and Stabilization Studies of ADN with AN Impurities in the Presence of Catalysts
2018 · Pratim Kumar, Rajiv Kumar, et al. · Lecture notes in mechanical engineering · 4
Performance estimation of hybrid rocket by varying the flow rate at multi-location swirl injector
2024 · Arpit Dubey, Rajiv Kumar, et al. · FirePhysChem · 2
Effect of Different Injectors on Performance of Hybrid Rocket Motor by Varying the L/D Ratio
2024 · Arpit Dubey, Rajiv Kumar, et al. · Lecture notes in mechanical engineering · 2
Effect of Protrusion on Combustion Stability of Hybrid Rocket Motor
2022 · Mengu Dinesh, Rajiv Kumar · Propellants Explosives Pyrotechnics · 2
Effect of Varying Secondary Swirl Injector Location on Performance of Hybrid Rocket
2025 · Arpit Dubey, Rajiv Kumar, et al. · Journal of Propulsion and Power · 1
Works count: 48
Citation count: 583
H-index: 13
I10-index: 15
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