-
61
Measurement report: Rocket-borne measurements of large ions in the mesosphere and lower thermosphere – detection of meteor smoke particles
Published 2025-01-01“…<p>We present mass spectroscopic in situ data from rocket flights of two improved ion mass spectrometers in the mesosphere and lower thermosphere region. …”
Get full text
Article -
62
A Novel Active Disturbance Rejection Control with a Super-Twisting Observer for the Rocket Launcher Servo System
Published 2021-01-01“…In this paper, a novel active disturbance rejection control (NADRC) with a super-twisting extended state observer (SESO) is utilized in the rocket launcher servo system. The main arguments in the shipborne rocket launcher system are control accuracy and antidisturbance ability, which are closely related to phase delay and bandwidth. …”
Get full text
Article -
63
-
64
-
65
London Rocket (<i>Sisymbrium irio</i> L.) as Healthy Green: Bioactive Compounds and Bioactivity of Plants Grown in Wild and Controlled Environments
Published 2024-12-01Subjects: “…London rocket…”
Get full text
Article -
66
Statement of the problem of designing a liquid rocket engine dual bell nozzle of the maximum thrust using the direct method of the calculus of variations
Published 2023-06-01“… A rocket engine with a standard single-section profiled nozzle provides maximum thrust only at a certain value of atmospheric pressure [1]. …”
Get full text
Article -
67
Short‐Period Concentric Traveling Ionospheric Disturbances Excited by the Launch of China's Long March 4B Rocket Detected by 1 Hz GNSS Data
Published 2022-06-01“…The CTIDs were most likely generated after the ignition of second‐stage rockets above the mesopause region.…”
Get full text
Article -
68
Safety Requirements Identification in Suborbital Payload Experiments
Published 2025-01-01Subjects: Get full text
Article -
69
Numerical Investigation of the Effect of Equivalent Ratio on Detonation Characteristics and Performance of CH<sub>4</sub>/O<sub>2</sub> Rotating Detonation Rocket Engine
Published 2025-01-01“…Equivalent ratio (ER) is an important factor affecting detonation characteristics and propulsion performance of rotating detonation rocket engine (RDRE). In this paper, the effects of different equivalent ratios detonation characteristics and thrust performance of methane-oxygen RDRE were studied by 2D numerical simulation. …”
Get full text
Article -
70
Emulation of ARISTOTLE and ROCKET AF trials in real-world atrial fibrillation patients results in similar efficacy and safety as original landmark trials: insights from the GARFIELD-AF registry
Published 2025-01-01“…Among ROCKET AF-eligible rivaroxaban users, HRs for rivaroxaban versus VKA were 0.90 (0.57 to 1.43), 0.92 (0.59 to 1.43) and 0.86 (0.69 to 1.08), respectively. …”
Get full text
Article -
71
Numerical Modeling and GNSS Observations of Ionospheric Depletions Due To a Small‐Lift Launch Vehicle
Published 2023-09-01Subjects: Get full text
Article -
72
Optimal Design of the Pitching Mechanism Considering the Influence of Erecting Angle Curves
Published 2024-12-01Subjects: “…Rocket launcher…”
Get full text
Article -
73
Design of modernized test bench for analysis of cooling systems with intensification under inertial forces field
Published 2019-04-01Subjects: “…liquid rocket engines…”
Get full text
Article -
74
Experimental study of cooling systems with intensification in field of inertial forces
Published 2019-10-01Subjects: “…liquid rocket engines…”
Get full text
Article -
75
Study of unusable liquid propellant residues evaporation processes parameters in the tanks of launch vehicle worked-off stage in microgravity
Published 2019-06-01Subjects: “…worked-off rocket stage…”
Get full text
Article -
76
-
77
Bringing Intelligence to the Edge for Structural Health Monitoring: The Case Study of the Z24 Bridge
Published 2024-01-01Subjects: “…MINImally RandOm Convolutional KErnel Transform (MiniRocket)…”
Get full text
Article -
78
Firing Control Optimization of Impulse Thrusters for Trajectory Correction Projectiles
Published 2015-01-01“…Further simulations show that the impact point dispersion is mainly influenced by the total impulse deployed, and the impulse, number, and firing interval need to be optimized to reduce the impact point dispersion of rockets. Live firing experiments with two trajectory correction rockets indicate that the firing control scheme works effectively.…”
Get full text
Article -
79
Optimization design of an acoustic cover layer for a cylindrical cavity based on porous materials
Published 2025-03-01“…During the launch and flight of carrier rockets, the acoustic and vibrational excitations generated by the external environment pose significant threats to their internal payloads. …”
Get full text
Article -
80
MUBEM & SAC: STEM Based Science and Nature Camp
Published 2019-07-01“…The participants found the opportunity to use telescopes, experience an extensive archaeological excavation, observe the near-nano size object with electron microscopes, construct a bridge like an engineer, and design artifacts like rockets and holograms during the camp. According to results, the science and nature camp supported participants’ STEM attitudes and participants' views on the science and nature camp were positive. …”
Get full text
Article