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Safety of a rotating detonation engine fed by acetylene – oxygen mixture launching stage
A multi-objective variable-specific impulse maneuvers optimization methodology
Investigation of interior ballistics and performance analysis of hydro-reactive motors
The use of detailed kinetics for modeling aerospace propulsion devices
Effect of ceramic nozzle on performance of pulsed plasma thruster
Numerical study of liquid propellants combustion for space applications
Feasibility analysis of solar thermal propulsion system with thermal energy storage
Thermodynamic cycle analysis of ramjet engines using magnesium-based fuel
Yuzhnoye's new liquid rocket engines as enablers for space exploration
Numerical study on operating characteristics of a magnesium-based fuel ramjet
Thermodynamic performance analysis of turbofan engine with a pulse detonation duct heater
Design and performance evaluation of a novel H2/O2 electro-chemical hybrid thruster
The thrust minimization problem and its applications
The thrust minimization problem and its applications
Global Optimization of Low-Thrust Interplanetary Trajectories Subject to Operational Constraints
Experimental study on the discharge of a xenon-assisted krypton Hall thruster
Eagleworks Laboratories: Advanced Propulsion Physics Research
Factors Affecting the Efficiency of Krypton Hall Thrusters
Method of continuation for optimization of interplanetary low-thrust trajectories
Method of continuation for optimization of interplanetary low-thrust trajectories
Mission Analysis for High Specific Impulse Deep Space Exploration
Influence of assumptions upon the parameters of multiphase products at chemical fuel combustion
Influence of assumptions upon the parameters of multiphase products at chemical fuel combustion
Calculation of tractive nozzle characteristics with altitude compensation
Calculation of tractive nozzle characteristics with altitude compensation
Nuclear Cryogenic Propulsion Stage for Near-Term Space Missions
Generalization of experimental data on two-phase critical efflux through axisymmetric channels
Generalization of experimental data on two-phase critical efflux through axisymmetric channels
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions
Solar Electric Propulsion Performance for Medlite and Delta Class Planetary Missions
Propellant-Less Thrust Generation - A Review
Design and Analysis of Rotating Detonation Wave Engine
Fuel-Rich Combustion with Ammonium Perchlorate Addition in a Staged Hybrid Rocket Engine
Radioisotope Electric Propulsion (REP): A Near-Term Approach to Nuclear Propulsion