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Interaction Behavior of Pulsejet Engines
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions
Utilization of Nonthermal Plasma in Pulse Detonation Engine Ignition
Shock-Initiated Combustion in an Airbreathing, Pulse Detonation Engine-Crossover System
Maximizing Lift-to-Drag and Thrust-to-Drag Ratios for Trimmed Hypersonic Vehicles
Effects of Propellant Slosh on Touchdown Stability for Landing Vehicles
100-kHz Coherent Raman Thermometry in a Free-Piston Shock Tube
to Mars: A Combined Robotic/Piloted Mars Mission
Optimal Midcourse Guidance for Dual-Pulse Rocket Using Pseudospectral Sequential Convex Programming
Automated Design of Propellant-Optimal, Low-Thrust Trajectories for Trojan Asteroid Tours
Near-Optimal Feedback Strategies Synthesized Using a Spatial Statistical Approach
Mitigating Time-Delay in Nonlinear Dynamics Inversion for Multirotor Unmanned Aerial Vehicles
Dynamic Features of Internal and External Flowfields of Pulsejet Engines
Aerodynamic Stabilization of a Finless Projectile with Active Nose Deflection
Active Valve Resonant Pulse Combustor for Pressure Gain Combustion Applications
Direct Thrust Measurement of an Electron Cyclotron Resonance Plasma Thruster
Characterization of Helicon Plasma Thruster Performance Operated for Various Rare Gas Propellants
Experimental Study of Pressure Gain Combustion with Hypergolic Rocket Propellants
Thrust Characteristics of High-Density Helicon Plasma Using Argon and Xenon Gases
Radar Terminal Descent Sensor Performance During Mars Science Laboratory Landing
Analytical Guidance Solutions for Spacecraft Planar Rephasing via Input Shaping
Minimum-Eigenvalue-Based Fault-Tolerant Adaptive Dynamic Control for Spacecraft
Effect of Ionic Liquid Composition on Colloid Thruster Emission and Thrust Performance
Low-Cost Laser Range-Measurement-Based Terrain-Following Concept and Error Analysis
Three-Electrode Plasma Synthetic Jet Actuator for High-Speed Flow Control
Collision-Inclusive Trajectory Optimization for Free-Flying Spacecraft
Feasibility Assessment of Rapid Earth–Mars Transfers Using High-Power Electric Propulsion
Real-Time Closed-Loop System Identification of a Quadcopter
Non-Premixed Burner-Attached Jet Flames in Crossflow Pulsed at Resonance Frequency
Time-Resolved Flowfield Measurements of Momentum-Driven Pulsed Transient Jets
Flow Rate Measurement Method for Gaseous Fuel Injection for Pulse Detonation Engines
Temperatures of Spark Kernels Discharging into Quiescent or Crossflow Conditions
Efficiency Characteristic of Plasma Synthetic Jet Actuator Driven by Pulsed Direct-Current Discharge
Adaptive State-Dependent Riccati Equation Control for Formation Reconfiguration in Cislunar Space
Effects of Copper Foam Wall/Obstacles on the Deflagration-to-Detonation Transition
Quaternion-Based Bang-Bang Attitude Stabilizer for Rotating Rigid Bodies
Smoked Foil on Deflagration-to-Detonation Transition
Detonation Transition Around Cylindrical Reflector of Pulse Detonation Engine Initiator
Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster
Flow Characterization of Heavy-Lift Helicopter Rear Fuselage with Pulsed Jets for Separation Control
Attitude Parameter Inspired Relative Motion Descriptions for Relative Orbital Motion Control
Starting Process of a Pulsed Jet as Seen by Schlieren Measurements