Results 201 to 210 of about 18,526 (302)
BLOOSTAR, The Enabler for More Efficient Satellites in Low Earth Orbit [PDF]
José Mariano López Urdiales +2 more
openalex +1 more source
A self‐sustaining solar photoelectrochemical cell (SS‐PEC) is developed to recover uranium from aqueous UO22+ with concurrent organic oxidation and electricity production. The monolithical photoanode directly captures electrons from organic compounds, leading to the oxidation of organic compounds and the decomposition of uranium‐organic complexes ...
Yumei Wang +7 more
wiley +1 more source
A Ku-Band Compact Offset Cylindrical Reflector Antenna with High Gain for Low-Earth Orbit Sensing Applications. [PDF]
Esmail BAF, Isleifson D, Shafai L.
europepmc +1 more source
Hollow poly(heptazine imide) spheres are prepared through a novel approach that integrates hard templating with ionothermal synthesis. This method enables precise control over surface area, pore volume, hydrophilicity, light absorption, band position, and metal composition. These tunable properties facilitate the customized design of semiconductors for
Lingli Ni +10 more
wiley +1 more source
Perspectives on the physics of late-type stars from beyond low earth orbit, the moon and mars. [PDF]
Mathur S, Santos ÂRG.
europepmc +1 more source
Multifunctional atomic layer deposited coatings and interface treatments enhance direct solar water splitting on GaAs/GaInP tandem cells. Optimized TiO2/Pt nanoparticle bilayers ensure durability and catalytic efficiency with minimal optical losses, while H2 plasma pretreatments maximize photovoltage and interfacial charge extraction.
Tim F. Rieth +8 more
wiley +1 more source
Orbital Reef and commercial low Earth orbit destinations-upcoming space research opportunities. [PDF]
Zea L +5 more
europepmc +1 more source
The effects of microgravity and space radiation on cardiovascular health: From low-Earth orbit and beyond. [PDF]
Patel S.
europepmc +1 more source
System Requirements for Low-Earth-Orbit Launch Using Laser Propulsion
R. J. Lawrence +3 more
openalex +2 more sources
Fuel-optimal low-earth-orbit maintenance
First-order solutions indicate that a forced Keplerian trajectory (FKT) obtained by thrust-drag cancellation is as fuel-efficient as a Hohmann transfer. Further analysis has shown that the FKT is not Mayer-optimal. Therefore there must exist another trajectory that matches or exceeds the efficiency of the Hohmann transfer.
openaire +1 more source

