This is our latest selection of worldwide publications and patents in english on Space Exploration, between many scientific online journals, classified and focused on space exploration, astronaut, cosmonaut, spacecraft, extravehicular activity, launch vehicle, space station, terraforming, asteroid belt, lunar module, space probe, Mars rover, space telescope, zero gravity, interstellar, astrobiology and exoplanet.
Launch system
Patent published on the 2026-07-02 in WO under Ref WO2026139948 by ISRAEL AEROSPACE IND LTD [IL] (Levy Oren [il], Gad Levi Oren [il])
Abstract: A launch system includes a launcher and a launch vehicle. The launch vehicle upper portion has a diameter greater than the lower portion, which includes a propulsion system. The launcher includes: a launch tube, a piston assembly, and an actuation system. The piston assembly is selectively movable along a piston axis, co-axial with the central axis of the launch tube, between two axial positions to thereby eject the launch vehicle from the launch tube. The piston assembly includes a piston membe[...]
Our summary: A launch system consists of a launcher and a launch vehicle. The launcher features a piston assembly that moves along a piston axis to eject the launch vehicle. An actuation system accelerates the piston assembly, providing the necessary launch force.
launch system, launch vehicle, piston assembly, actuation system
Patent
Reusable launch vehicle with auxiliary propellant tanks for non-ascent burns
Patent published on the 2026-07-02 in US under Ref US20260184442 by BLUE ORIGIN LLC [US] (Grayson Gary [us], Wuerl Adam M [us], Degenhardt David [us])
Abstract: A reusable launch vehicle comprising auxiliary tanks for non-ascent burns, such as orbital maneuver burns, reorientation burns, deorbit burns, or landing burns, and/or power generation. The auxiliary tanks may provide propellants for an orbital maneuvering system, an orbital reaction control system, a reentry reaction control system, and/or a power generation system. The tanks are configured to maintain cryogenic properties of auxiliary fuel and auxiliary oxidizer for the duration of the mission[...]
Our summary: The content describes a reusable launch vehicle designed with auxiliary propellant tanks for non-ascent burns. These tanks support various functions, including orbital maneuvers and power generation, while maintaining cryogenic properties. The configuration of the tanks allows for optimal positioning and insulation of cryogenic fluids during the mission.
reusable launch vehicle, auxiliary propellant tanks, non-ascent burns, cryogenic properties
Patent
System and method for reducing the data volume downlinked from spacecraft to ground stations
Patent published on the 2026-06-24 in EP under Ref EP4765800 by UBOTICA TECH LIMITED [IE] (Doody John [ie], Dunne Aubrey [ie])
Abstract: [0001] Systems and methods for reducing the data volume downlinked from a spacecraft to a ground station are disclosed. A processing system onboard the spacecraft captures image data from one or more imaging sensors and forms an image stack of spectral bands that is partitioned into tile stacks corresponding to common spatial regions. A trained artificial intelligence model performs inference on each tile stack to generate a quantitative tile stack score indicative of predicted usefulness for on[...]
Our summary: The system reduces data volume transmitted from spacecraft to ground stations. It captures image data and partitions it into tile stacks for processing. AI evaluates each tile stack to determine the appropriate compression or discarding action before transmission.
data compression, spacecraft, artificial intelligence, image processing
Patent
System and method for autonomous support of extravehicular activity operations in space
Patent published on the 2026-06-18 in US under Ref US20260167362 by MACDONALD DETTWILER AND ASS INC [CA] (Sorocky Michael Joseph [ca], Langley Christopher Stewart [ca], Watson William [us], Arnold Katherine [ca], Caldwell Jack Austin [ca])
Abstract: [0000] A system and method for autonomously supporting extravehicular activity (“EVA”) on a spacecraft is provided. The system includes: a robotic arm for moving an EVA crew member on a robotic arm to and from a worksite; an autonomy processing device configured to: execute a collision avoidance module that detects a potential collision situation based on telemetry received from sensors of the robotic arm, wherein the collision avoidance module includes preconfigured collision models represe[...]
Our summary: The system provides autonomous support for extravehicular activities on spacecraft. It includes a robotic arm for crew movement and an autonomy processing device for collision avoidance. The device detects unexpected obstacles during the robotic arm s motion using real-time image data.
autonomous systems, extravehicular activity, robotic arm, collision avoidance
Patent
Systems, devices, and methods for spacecraft connections
Patent published on the 2026-06-17 in EP under Ref EP4759726 by MACDONALD DETTWILER & ASSOCIATES CORP [CA] (Dame SÉbastien [ca], Suthertown Emily Mackay [ca])
Abstract: Provided is a system, method and device for spacecraft connections. The system includes a first spacecraft including a structural connector that provides structural support and alignment to a second structural connector and an electrical connector that electrically connects the spacecraft platform to a launch vehicle and/or a second spacecraft. The electrical connector includes a first connector pad that mates with a second connector pad. The electrical connector is absent a connection force inh[...]
Our summary: The system enables connections between spacecraft using structural and electrical connectors. The structural connector ensures proper alignment and support. The electrical connector operates without inherent connection force, allowing for flexible attachment.
spacecraft connections, structural connector, electrical connector, launch vehicle
Patent
Systems and methods for jitter minimization by stepper motor control
Patent published on the 2026-05-27 in EP under Ref EP4749911 by MACDONALD DETTWILER & ASSOCIATES CORP [CA] (Larouche Steve [ca], Chambon JÉrÉmy [ca])
Abstract: Provided herein are systems and methods for minimizing jitter. A method for minimizing jitter for at least one sensitive component on a spacecraft includes receiving a rotary actuator speed command indicating a rotary actuator speed for a stepper motor on the spacecraft, setting a stepping mode of the stepper motor to one of a first stepping mode and second stepping mode based on a preconfigured data structure which encodes a corresponding stepping mode for the rotary actuator speed based on a p[...]
Our summary: The content discusses systems and methods for minimizing jitter in spacecraft components. It involves controlling the stepping mode of a stepper motor based on rotary actuator speed commands. The approach aims to keep harmonics outside of jitter-sensitive frequency bands.
jitter minimization, stepper motor control, spacecraft systems, rotary actuator speed
Patent
yet another quantum quantizer design space exploration of quantum gate sets using novelty search
Published on 2026-04-09 by Aritra Sarkar, Akash Kundu, Matthew Steinberg, Sibasish Mishra, Sebastiaan Fauquenot, Tamal Acharya, Jaros?aw A Miszczak and Sebastian Feld @IOP SCIENCE
Abstract: The standard model of quantum computation is based on quantum circuits, where the number and quality of the quantum gates composing the circuit influence the runtime and fidelity of the computation. The fidelity of the decomposition of quantum algorithms, represented as unitary matrices, to bounded depth quantum circuits depends strongly on the set of gates available for the decomposition routine. To investigate this dependence, we explore the design space of discrete quantum gate sets and prese[...]
Our summary: This study explores the design space of quantum gate sets using a software tool called YAQQ. It evaluates gate sets based on circuit depth, process fidelity, and novelty. The findings highlight optimized gate sets for quantum algorithms and practical applications in error correction and instruction set design.
quantum gates, novelty search, circuit decomposition, quantum fidelity
Publication
Coverage Ratio–Based Evaluation of Antenna Omnidirectionality for a Pair of Microstrip Patch Antennas on a 6U CubeSat
Published on 2026-02-03 by Daisuke Nakayama, Kei Sano, Rin Sato, Tohlu Matsushima, Yuki Fukumoto @MDPI
Abstract: CubeSat missions increasingly rely on microwave-band communication systems, whose antennas often exhibit directional radiation patterns. As a result, multiple antennas are commonly used to improve coverage; however, a quantitative method to evaluate their performance across all spacecraft attitudes has been lacking. This paper introduces the Coverage Ratio of CubeSat Attitude (CRCA), a metric that quantifies the proportion of orientations for which the antenna gain exceeds a required threshold. [...]
Our summary: This paper presents the Coverage Ratio of CubeSat Attitude (CRCA) metric to evaluate antenna performance across spacecraft orientations. It demonstrates the CRCA using the S-band command antenna system of the 6U CubeSat VERTECS. The study compares antenna configurations and shows the effectiveness of the proposed metric in assessing communication performance under varying attitudes.
Coverage Ratio, Antenna Omnidirectionality, CubeSat, Microwave Communication
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