Propagation of strong shock waves in a non-ideal gas
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.03.039
Nanosatellites swarm deployment using decentralized differential drag-based control with communicational constraints
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.02.006
LES of primary breakup of pulsed liquid jet in supersonic crossflow
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.10.043
A mathematical model for the separation behavior of a split type low-shock separation bolt
来源期刊:Acta AstronauticaDOI:10.1016/j.actaastro.2019.07.035
Osteoclast-derived exosomes inhibit osteogenic differentiation through Wnt/β-catenin signaling pathway in simulated microgravity model
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.08.044
Survey on key techniques of rocket-based combined-cycle engine in ejector mode
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.07.016
Global search for periodic orbits in the irregular gravity field of a binary asteroid system
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.10.014
Icy giant planet exploration: Are entry probes essential?
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.06.020
Rotating detonation engines with two fuel orifice schemes
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.05.035
Near-term interstellar probe: First step
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.06.013
Growing blood vessels in space: Preparation studies of the SPHEROIDS project using related ground-based studies
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.03.074
Mixing augmentation mechanism induced by the dual injection concept in shcramjet engines
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.11.019
Effect of blockage ratio on the existence of multiple waves in rotating detonation engine
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.08.007
Effect of SiO2 crystal structure on the stability of polymer composites exposed to vacuum ultraviolet radiation
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.11.017
A linear model for relative motion in an elliptical orbit based on a spherical coordinate system
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.01.016
The orbit deployment strategy of OOS system for refueling near-earth orbit satellites
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.02.001
Modeling and control of a nonlinear coupled spacecraft-fuel system
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.06.029
Glide trajectory optimization for hypersonic vehicles via dynamic pressure control
来源期刊:Acta AstronauticaDOI:10.1016/j.actaastro.2019.08.012
Design of a Film Cooled Dual-Bell Nozzle
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.05.056
Velocity-free sliding mode control for spacecraft with input saturation
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.10.045
Principles for a practical Moon base
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.04.018
Optimal low-thrust hyperbolic rendezvous for Earth-Mars missions
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.02.020
Optical Analysis of the Liquid Layer Combustion of Paraffin-based Hybrid Rocket Fuels
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.05.059
Search-based method optimization applied to bi-impulsive orbital transfer
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.03.015
A compact C-Band CP-SAR microsatellite antenna for Earth Observation
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.01.030
Novel osculating flowfield methodology for wide-speed range waverider vehicles across variable Mach number
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.05.056
Mars atmospheric entry guidance for optimal terminal altitude
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.12.001
Large eddy simulation on using a cavity-jet controller for supersonic blunt base mixing layer control
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.05.019
Role of aerodome in pulsation/oscillation control and aeroheating reduction
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.05.030
International coordination on planetary defence: The work of the IAWN and the SMPAG
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.07.023
Structure Development of the HP3 Instrument Support System for the Mars Mission InSight
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.06.035
Experimental evaluation of thermoelectric generators for nanosatellites application
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.05.053
Precision characterization of the TESS CCD detectors: Quantum efficiency, charge blooming and undershoot effects
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.04.016
Experimental investigation of the effects of chamber length and boron content on boron-based gel fuel ramjet performance
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.03.076
The feasibility of deflecting asteroid 2017 PDC using neutral beam propulsion
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.03.057
A graphical tool to design two-ways human Mars missions
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.03.035
How holistic interactive experience can inspire the younger generation through voluntary engagement
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.05.041
A space surveillance satellite for cataloging high-altitude small debris
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.01.003
Proximity scenario design for geostationary rendezvous with collocated satellite avoidance
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2018.11.004
Orbital lifetime and collision risk reduction for inclined geosynchronous disposal orbits
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.05.021
Evacuation method and outgassing rate of a lunar regolith simulant for deep drilling tests
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.01.022
Development of shape monitoring system using SMA dipole antenna on a deployable membrane structure
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.04.007
A new nonlinear Type3-PLL with noise rejection and fast locking performance in tracking telemetry and command systems
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.01.006
Performance assessment of supersonic and hypersonic intake systems with nano-particle injection
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.02.008
Flowfield structures of pylon-aided fuel injection into a supersonic crossflow
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.06.022
SETI in Russia, USSR and the post-Soviet space: a century of research
来源期刊:Acta AstronauticaDOI:10.1016/j.actaastro.2019.04.030
Lifesaving rockets in Sweden. A century of operation
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.06.018
Geometrical characteristics of optimal transfer between noncoplanar elliptical orbits
来源期刊:Acta AstronauticaDOI:10.1016/j.actaastro.2019.09.024
Design of distant retrograde orbits based on a higher order analytical solutiont
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.01.039
Thermal simulation of drilling into lunar rock simulant by discrete element method
来源期刊:Acta AstronauticaDOI:10.1016/J.ACTAASTRO.2019.05.002