| 1 |
Hypergolic ignition delay studies of solidified ethanol fuel with hydrogen peroxide for hybrid rockets
John J, Nandagopalan P, Baek SW, Cho SJ
Combustion and Flame, 212, 205, 2020 |
| 2 |
Radiation heat transfer in ablating boundary layer combustion theory used for hybrid rocket motor analysis
Budzinski K, Aphale SS, Ismael EK, Surina G, DesJardin PE
Combustion and Flame, 217, 248, 2020 |
| 3 |
Regression Rate Characterization of HTPB-Paraffin Based Solid Fuels for Hybrid Rocket
Mahottamananda SN, Kadiresh NP, Pal Y
Propellants Explosives Pyrotechnics, 45(11), 1755, 2020 |
| 4 |
Regression Rate Characterization of HTPB-Paraffin Based Solid Fuels for Hybrid Rocket
Mahottamananda SN, Kadiresh NP, Pal Y
Propellants Explosives Pyrotechnics, 45(11), 1755, 2020 |
| 5 |
Rheology of solid-like ethanol fuel for hybrid rockets: Effect of type and concentration of gellants
John J, Nandagopalan P, Baek SW, Miglani A
Fuel, 209, 96, 2017 |
| 6 |
Mechanical Modifications of Paraffin-based Fuels and the Effects on Combustion Performance
Tang Y, Chen SH, Zhang W, Shen RQ, DeLuca LT, Ye YH
Propellants Explosives Pyrotechnics, 42(11), 1268, 2017 |
| 7 |
Thermal characterizations of the paraffin wax/low density polyethylene blends as a solid fuel
Kim S, Moon H, Kim J
Thermochimica Acta, 613, 9, 2015 |
| 8 |
Thermal characteristics of an N2O catalytic igniter with metal foam for hybrid rocket motors
You WJ, Moon HJ, Jang SP, Kim JK
International Journal of Heat and Mass Transfer, 66, 101, 2013 |
