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Yuzhnoye's new liquid rocket engines as enablers for space exploration
WIOBSS: The Chinese low-power digital ionosonde for ionospheric backscattering detection
Watching the Swiss: A network approach to rural and exurban public transport
Walkability inequity in Los Angeles: Uncovering the overlooked role of micro-level features
Two-tangent-impulse flyby of space target from an elliptic initial orbit
Trajectory determination at Muon Impact Tracer and Observer (MITO) using artificial neural networks
Three-impulse point return orbit design for the manned lunar high-latitude exploration mission
The use of detailed kinetics for modeling aerospace propulsion devices
Thermodynamic performance analysis of turbofan engine with a pulse detonation duct heater
Thermodynamic cycle analysis of ramjet engines using magnesium-based fuel
The effects of experience in the A380 duty free showcase on customer behaviors
The design of optimal guidance law with multi-constraints using block pulse functions
Ten-year transient luminous events and Earth observations of FORMOSAT-2
Temporal and spatial structure of “caviton” signal scattered by modified ionosphere
Suboptimal LQR-based spacecraft full motion control: Theory and experimentation
Stabilization and steering of a parabolic laser thermal thruster with an ignition device
“Solitary” Trans-Ionospheric Pulse Pairs onboard of the microsatellite “Chibis-M”
Solar wind-driven electron radiation belt response functions at 100-min time scales
Solar irradiance, climatic indicators and climate change – An empirical analysis
Simple solution to optimal cotangential transfer between coplanar elliptic orbits
Safety of a rotating detonation engine fed by acetylene – oxygen mixture launching stage
Revisiting the fuel-optimal four-impulse rendezvous problem near circular orbits
Review and prospect of guidance and control for Mars atmospheric entry
Real-world battery duty profile of a neighbourhood electric vehicle
Reachable domain with a single coplanar impulse considering the target-visit constraint
Reachable domain of spacecraft with a single tangent impulse considering trajectory safety
Radioisotope electric propulsion (REP): A near-term approach to nuclear propulsion
Pulse volume discharge behind shock wave in channel flow with obstacle
Project Lyra: Catching 1I/‘Oumuamua–Using Nuclear Thermal Rockets
Preliminary study of a pulse normal detonation wave engine
Performance comparison between two different injector configurations in a hybrid rocket
Optimum design of power-limited propulsion systems with application to fast Earth-to-Mars transfer
Optimal transfer between elliptic orbits with three tangential impulses