Rudresh M,
Naresh D C,
Debadatta MİSHRA
Design and Analysis of Combustion Chamber for HAN Based Mono Propulsion System Thruster for Spacecraft Application
Design and Analysis of Combustion Chamber for HAN Based Mono Propulsion System Thruster for Spacecraft Application
International Journal of Aviation Science and Technology
2020-Cilt: 01 - Sayı: 02
66-70
Hydroxyl Ammonium Nitrate,
Computational Fluid Dynamics,
Attitude and Orbit Control System,
Mono Propellant Thrusters,
Combustion
110
85