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Damping or gain? -The critical roles aluminum plays in the SRM stability
Experimental study on the discharge of a xenon-assisted krypton Hall thruster
Joint runway–gate assignment based on the Branch-and-Price algorithm
Measurement of ablation impulse and direction with oblique laser-pulse irradiation
A multi-objective variable-specific impulse maneuvers optimization methodology
Minimum-fuel two-impulse transfer between coplanar noncoaxial elliptical orbits
Trajectory determination at Muon Impact Tracer and Observer (MITO) using artificial neural networks
Walkability inequity in Los Angeles: Uncovering the overlooked role of micro-level features
A miniaturised fetch rover concept for Mars sample return
Reachable domain with a single coplanar impulse considering the target-visit constraint
The use of detailed kinetics for modeling aerospace propulsion devices
Investigation on operational stability of a pulsed plasma thruster with a pressure probe
Feasibility analysis of solar thermal propulsion system with thermal energy storage
Constrained optimization of n-impulse periodic close encounter orbits for inspection missions
Measuring volatility spillover effects in dry bulk shipping market
A satellite formation to display pixel images from the sky: Mission design and control algorithms
Pulse volume discharge behind shock wave in channel flow with obstacle
A maximum a posteriori estimation based method for estimating pulse time delay
On development and use of rockets for Mars atmosphere sounding
Safety of a rotating detonation engine fed by acetylene – oxygen mixture launching stage
Delta-V and ground metric investigations for responsive satellite formation flying
Collision avoidance maneuver optimization with a multiple-impulse convex formulation
An effective means of drag reduction in high enthalpy flow through unsteady energy deposition
Impact of neutron energy on asteroid deflection performance
A two-stage thermally-coupled pulse tube cryocooler working at 35 K for space application
An analysis of X-ray pulsar navigation accuracy in Earth orbit applications
Capabilities and limitations of existing hypersonic facilities
In-flight testing of the injection of the LISA Pathfinder test mass into a geodesic
Three-impulse point return orbit design for the manned lunar high-latitude exploration mission