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Aerospace, Volume 12, Issue 6

2025 June - 113 articles

Cover Story: Aviation is key to global interconnectivity. To maintain its benefits while reducing emissions, future aircraft will require radical redesigns and novel technologies. Hydrogen aircraft offer a promising path to emissions reduction, with entry into service targeted for 2035. Achieving this goal demands rapid certification despite immature designs and unestablished processes. Accelerating progress requires early regulatory analysis and definition of technology and operational options. The CONCERTO project addressed this by analysing and weighting these elements, resulting in a Generic Concept at CRL1. This paper outline major system changes, integration challenges, and operational shifts needed to enable this concept’s flight. View this paper
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Articles (113)

  • Article
  • Open Access
1 Citations
1,539 Views
26 Pages

This study employs Direct Numerical Simulation (DNS) to investigate the flow and heat transfer characteristics in a compressor blade passage at five Reynolds numbers (Re=1.091×105, 1.229×105, 1.367×105, 1.506×105, and 1.645&ti...

  • Article
  • Open Access
1,756 Views
28 Pages

With the enhancement of thermodynamic cycle parameters and heat dissipation constraints in aero-engines, effective thermal management has become a critical challenge to ensure safe and stable engine operation. This study developed a transient tempera...

  • Article
  • Open Access
1,577 Views
24 Pages

To commercialize supersonic and hypersonic passenger aircraft and reusable spaceplanes, we are developing a small-scale supersonic flight experiment vehicle as a flying testbed for technical demonstrations in high-speed flight environments. This expe...

  • Article
  • Open Access
1 Citations
3,386 Views
15 Pages

This study shows a comprehensive simulation to assess and enhance the throughput capacity of unmanned air system vertiports, one of the most essential elements of urban air mobility ecosystems. The framework integrates dynamic grid-based spatial mana...

  • Article
  • Open Access
1 Citations
2,674 Views
35 Pages

Certifying novel VTOL aircraft handling qualities (HQs) may be challenging, relying on costly and high-risk flight testing. This paper presents a methodology to establish the credibility of flight simulation models for certification by simulation, ai...

  • Article
  • Open Access
1 Citations
755 Views
20 Pages

Targeting the nonlinear issues of the canard dual-spin aircraft, which relies on the high-speed rotation of the afterbody for flight stability and achieves trajectory correction by adjusting the roll angle of the low-speed rotating forebody to alter...

  • Article
  • Open Access
650 Views
26 Pages

Previous works by our group evidenced stability problems associated with flight control law design for flexible aircraft regarding gain scheduling. This paper proposes an output feedback fuzzy-based gain scheduling approach to adequate closed-loop re...

  • Article
  • Open Access
2,784 Views
35 Pages

Conceptual Design of a Low-Cost Class-III Turbofan-Based UCAV Loyal Wingman

  • Savvas Roussos,
  • Eleftherios Karatzas,
  • Vassilios Kostopoulos and
  • Vaios Lappas

The rapid evolution of military technology has led to an increased interest in Unmanned Combat Aerial Vehicles (UCAVs). This research focuses on the conceptual design of a low-cost, turbofan-powered UCAV, specifically a Class-III aircraft as defined...

  • Article
  • Open Access
1 Citations
1,164 Views
39 Pages

Predictive maintenance in commercial aviation demands highly reliable and robust models, particularly for critical components like carbon brakes. This paper addresses two primary concerns in modeling carbon brake wear for distinct aircraft variants:...

  • Article
  • Open Access
1 Citations
1,978 Views
33 Pages

Hydrogen-powered aircraft constitute a transformative innovation in aviation, motivated by the imperative for sustainable and environmentally friendly transportation solutions. This paper aims to concentrate on the design of hydrogen powertrains empl...

  • Article
  • Open Access
686 Views
25 Pages

Two-Stage Uncertain UAV Combat Mission Assignment Problem Based on Uncertainty Theory

  • Haitao Zhong,
  • Rennong Yang,
  • Aoyu Zheng,
  • Mingfa Zheng and
  • Yu Mei

Based on uncertainty theory, this paper studies the problem of unmanned aerial vehicle (UAV) combat mission assignment under an uncertain environment. First, considering both the target value, which is the combat mission benefit gained from attacking...

  • Article
  • Open Access
1 Citations
1,221 Views
24 Pages

A Multi-Scale Airspace Sectorization Framework Based on QTM and HDQN

  • Qingping Liu,
  • Xuesheng Zhao,
  • Xinglong Wang,
  • Mengmeng Qin and
  • Wenbin Sun

Airspace sectorization is an effective approach to balance increasing air traffic demand and limited airspace resources. It directly impacts the efficiency and safety of airspace operations. Traditional airspace sectorization methods are often based...

  • Article
  • Open Access
2 Citations
1,474 Views
17 Pages

Aviation safety analysis increasingly relies on extracting actionable insights from narrative incident reports to support risk identification and improve operational safety. Topic modeling techniques such as Probabilistic Latent Semantic Analysis (pL...

  • Review
  • Open Access
8 Citations
21,808 Views
78 Pages

An Overview of CubeSat Missions and Applications

  • Konstantinos-Panagiotis Bouzoukis,
  • Georgios Moraitis,
  • Vassilis Kostopoulos and
  • Vaios Lappas

The proliferation of CubeSats in Earth orbit has accelerated dramatically in recent years, with projections indicating continued growth in the coming decades. This review examines the evolution of CubeSat applications, from basic technology demonstra...

  • Article
  • Open Access
1,739 Views
17 Pages

Vacuum arc thrusters (VATs) have recently gained significant interest as a micro-propulsion system due to their scalability, low cost, storability, and small form factor. While VATs offer an attractive propulsion solution for CubeSats, conventional p...

  • Article
  • Open Access
1 Citations
698 Views
28 Pages

To describe the fouling characteristics of compressor blades, fouling is categorized into dense and loose layers to characterize thickness and rough structures. An uncertainty model for dense fouling layer thickness distribution is constructed using...

  • Article
  • Open Access
3 Citations
1,687 Views
17 Pages

The failure mode and effect analysis (FMEA) method, which estimates the risk levels of systems or components solely based on the multiplication of simple risk rating indices, faces several limitations. These include the risk of inaccurate risk level...

  • Article
  • Open Access
1 Citations
940 Views
20 Pages

An Aeroelastic Solution Method Using an Implicit Dynamic Approach

  • Weiji Wang,
  • Wei Qian,
  • Zheng Chen and
  • Xinyu Ai

This paper presents an innovative aeroelastic solution method called the implicit dynamic approach (IDA). The IDA is a novel technique implemented to address the complexities of structural displacement and fluid–structure interactions. At the c...

  • Article
  • Open Access
1,367 Views
26 Pages

Airline networks are becoming increasingly complex, particularly at mega-hub airports characterized by high transit volumes. Effective schedule design and fleet assignment are critical for an airline, as they directly influence passenger connectivity...

  • Review
  • Open Access
1 Citations
5,107 Views
12 Pages

Advances in the field of asteroid dynamics continue to yield new knowledge regarding the behavior and characteristics of asteroids, allowing unprecedented levels of accuracy for predicting trajectories and contributing to impact avoidance strategies....

  • Article
  • Open Access
1 Citations
2,388 Views
24 Pages

The accurate and reliable positioning of unmanned aerial vehicles (UAVs) in urban environments is crucial for urban air mobility (UAM) application, such as logistics, surveillance, and disaster management. However, global navigation satellite systems...

  • Article
  • Open Access
829 Views
23 Pages

Interactive Maintenance of Space Station Devices Using Scene Semantic Segmentation

  • Haoting Liu,
  • Chuanxin Liao,
  • Xikang Li,
  • Zhen Tian,
  • Mengmeng Wang,
  • Haiguang Li,
  • Xiaofei Lu,
  • Zhenhui Guo and
  • Qing Li

A novel interactive maintenance method for space station in-orbit devices using scene semantic segmentation technology is proposed. First, a wearable and handheld system is designed to capture images from the astronaut in the space station’s fr...

  • Article
  • Open Access
892 Views
25 Pages

Slat noise poses a significant challenge during aircraft landing. Slat gap filler (SGF) technology has shown promise in mitigating slat noise, yet its noise reduction mechanisms and characteristics remain unclear. This study numerically investigates...

  • Article
  • Open Access
1 Citations
850 Views
20 Pages

Autonomous aerial refueling (AAR) technology is of crucial importance in the aviation field. Accurately predicting the position of the refueling drogue is a core challenge in implementing this technology. An innovative method of a physics-informed ne...

  • Article
  • Open Access
1 Citations
2,054 Views
32 Pages

This paper addresses the real-time trajectory generation problem for hypersonic glide vehicles (HGVs) during atmospheric entry, subject to complex constraints including aerothermal limits, actuator bounds, and no-fly zones (NFZs). To achieve efficien...

  • Article
  • Open Access
836 Views
25 Pages

A Novel Curve-and-Surface Fitting-Based Extrapolation Method for Sub-Idle Component Characteristics of Aeroengines

  • Yibo Cui,
  • Tianhong Zhang,
  • Zhaohui Cen,
  • Younes Al-Younes and
  • Elias Tsoutsanis

The component characteristics of an aeroengine below idle speed are fundamental for start-up process simulations. However, due to experimental limitations, these characteristics must be extrapolated from data above idle speed. Existing extrapolation...

  • Article
  • Open Access
1,340 Views
19 Pages

Combustion instability is an abnormal working state that often occurs in advanced solid rocket motors (SRMs), which can arouse pressure oscillations, increase the risk of mission failure, and even cause structural damage. In this paper, a numerical s...

  • Article
  • Open Access
2 Citations
2,763 Views
14 Pages

Crosslinked phenolic resin was prepared using hexamethylenetetramine (HMTA) as a crosslinking agent in hydrochloric acid solution. The ablation-heat-resistant material was prepared by a pressure-assisted RTM (resin transfer molding) process with rein...

  • Article
  • Open Access
1,872 Views
22 Pages

Modeling Microgravity Using Clinorotation in a Microfluidic Environment: A Numerical Approach

  • João Fernandes,
  • Dara Machado,
  • Graça Minas,
  • Susana O. Catarino and
  • Diana Pinho

Microgravity simulation is essential for studying particle dynamics in space-related applications where traditional gravitational effects are absent. This study presents a numerical investigation of particle behavior in a clinostat-driven microfluidi...

  • Article
  • Open Access
747 Views
19 Pages

Shell-Stripping Mechanism of Red Sandstone Under Hypervelocity Impact with Aluminum Spheres

  • Yizhe Liu,
  • Quanyu Jiang,
  • Zishang Liu,
  • Minqiang Jiang,
  • Yadong Li,
  • Zhenghua Chang,
  • Kun Zhang and
  • Bingchen Wei

To investigate the size effect on fragmentation phenomena during hypervelocity impact, scaled experiments were conducted using a 30 mm smooth-bore ballistic range (DBR30) driven by a detonation-driven two-stage launching system. Unique stripping of s...

  • Article
  • Open Access
1,084 Views
22 Pages

Film Cooling Performance and Superposition Method of an Actual Turbine Vane at High Freestream Turbulence

  • Peng Chu,
  • Yongfeng Sui,
  • Bin Dai,
  • Jibing Lan,
  • Wenyang Shao,
  • Binbin Xue,
  • Xiliang Xu and
  • Zhenping Feng

This study aims to enhance the understanding of film cooling performance in an actual turbine vane by investigating influencing factors and developing more precise numerical prediction methods. Pressure sensitive paint (PSP) testing and Reynolds-Aver...

  • Article
  • Open Access
1,503 Views
23 Pages

The air transportation system is composed of multiple elements and belongs to a complex socio-technical system. It is difficult to assess the risk of an aircraft fault because it could constantly change during operation and is influenced by numerous...

  • Article
  • Open Access
1,303 Views
21 Pages

To address the interception problem against maneuvering targets, this paper proposes a multi-agent cooperative guidance law based on a multi-directional interception formation. A three-dimensional agent–target engagement kinematics model is est...

  • Article
  • Open Access
1,010 Views
20 Pages

Fused filament fabrication (FFF) is a 3D printing technology that has been successfully demonstrated aboard the International Space Station (ISS), proving its suitability for space applications. In this study, we aimed to apply FFF to the 3D printing...

  • Article
  • Open Access
2 Citations
1,112 Views
33 Pages

As air transportation demand continues to rise, congestion in air route networks has seriously compromised the safe and efficient operation of air traffic. Few studies have examined the spatiotemporal characteristics of congestion propagation under d...

  • Article
  • Open Access
1,119 Views
19 Pages

Demand-Driven Evaluation of an Airport Airtaxi Shuttle Service for the City of Frankfurt

  • Fabian Morscheck,
  • Christian Kallies,
  • Enno Nagel and
  • Rostislav Karásek

The CORUS-XUAM project defined three two-way U-space corridors linking Frankfurt Airport’s Terminal 2 on the city outskirts with the city-center Trade Fair. These corridors avoid the approach cones of the northern and central runways and bypass...

  • Article
  • Open Access
1 Citations
1,809 Views
20 Pages

With the rapidly increasing number of satellites and orbital debris, collision avoidance and reentry prediction are very important for space situational awareness. A precise orbital prediction through orbit determination is crucial to enhance the spa...

  • Article
  • Open Access
985 Views
16 Pages

Current deformation modeling theories for aircraft thin-walled components in riveting assembly typically assume uniform rivet interference. However, engineering practice shows that rivet interference is non-uniform, and such interference directly aff...

  • Article
  • Open Access
1,198 Views
24 Pages

The bistable laminated structure is widely used in many fields due to its unique deformation characteristics. In practical engineering, laminates under different structural constraints will exhibit different steady-state deformation characteristics....

  • Article
  • Open Access
1,343 Views
26 Pages

This paper investigates the design of optimal low-thrust transfers between relative planar and spatial quasi-satellite orbits (QSOs) in the Earth–Moon system under the Circular Restricted Three-Body Problem (CR3BP). A key contribution is the ad...

  • Article
  • Open Access
1 Citations
992 Views
20 Pages

Predicting Landing Position Deviation in Low-Visibility and Windy Environment Using Pilots’ Eye Movement Features

  • Xiuyi Li,
  • Yue Zhou,
  • Weiwei Zhao,
  • Chuanyun Fu,
  • Zhuocheng Huang,
  • Nianqian Li and
  • Haibo Xu

Eye movement features of pilots are critical for aircraft landing, especially in low-visibility and windy conditions. This study conducts simulated flight experiments concerning aircraft approach and landing under three low-visibility and windy condi...

  • Article
  • Open Access
1,501 Views
25 Pages

This study conducted a basic analysis of the supply and demand of aeronautical data communications, focusing on trajectory-based operation (TBO), which is one of the methods used for improving the efficiency of air traffic in the digital transformati...

  • Article
  • Open Access
1 Citations
990 Views
18 Pages

Aiming at the problems of excessive dependence on manual operations, unquantifiable parameters, low hoisting efficiency, and low level of automation and informatization in the lifting process of spacecraft, a novel cable-driven parallel automatic lev...

  • Article
  • Open Access
1 Citations
1,545 Views
19 Pages

To address the issue of misclassification and diminished accuracy that is prevalent in existing intent recognition models for non-cooperative spacecraft due to the omission of environmental influences, this paper presents a novel recognition framewor...

  • Review
  • Open Access
3 Citations
26,620 Views
29 Pages

A Review of Aerospike Nozzles: Current Trends in Aerospace Applications

  • Isaac Ramirez Cardenas,
  • Santiago Laín and
  • Omar Dario Lopez

The aerospike nozzle has emerged as a revolutionary technology in rocket propulsion, overcoming the limitations of conventional nozzles by dynamically adjusting the expansion of exhaust gases according to ambient pressure. This results in greater eff...

  • Article
  • Open Access
3 Citations
2,157 Views
29 Pages

In lunar exploration missions, rovers must navigate multiple waypoints within strict time constraints while avoiding dynamic obstacles, demanding real-time, collision-free path planning. This paper proposes a digital twin-enhanced hierarchical planni...

  • Article
  • Open Access
2 Citations
1,249 Views
17 Pages

This study presents a design approach for a uniform porous surface to control laminar-to-turbulent transition in hypersonic boundary layers. The focus is on suppressing the Mack second mode, which is a dominant instability in hypersonic boundary laye...

  • Feature Paper
  • Article
  • Open Access
868 Views
16 Pages

An Investigation of the Flashing Process of Liquid Xenon in a Refueling Pipe

  • Zongyu Wu,
  • Chao Jiang,
  • Kai Li,
  • Yiyong Huang,
  • Guangyu Li and
  • Yun Cheng

To investigate the phenomenon of liquid xenon flashing in a filling pipeline, the two-phase flow in a pipe is calculated and analyzed by using a one-dimensional homogeneous equilibrium model (HEM) and a two-dimensional mixture model. The distribution...

  • Article
  • Open Access
984 Views
19 Pages

Aircraft and fixed-wing drones, designed to perform vertical take-off and landing (VTOL), often incorporate unconventional configurations that offer unique capabilities but simultaneously pose significant challenges in flight mechanics modeling, whos...

  • Article
  • Open Access
1 Citations
3,572 Views
14 Pages

Space Demonstration of All-Solid-State Lithium-Ion Batteries Aboard the International Space Station

  • Yu Miyazawa,
  • Takanobu Shimada,
  • Tetsuhito Fuse,
  • Shuhei Shimada,
  • Sousuke Nishiura,
  • Hidetake Okamoto,
  • Tetsuya Okawa,
  • Takeshi Hoshino,
  • Osamu Kawasaki and
  • Hitoshi Naito

All-solid-state lithium-ion batteries (ASSBs) have a wide operating temperature range (−40 °C to +120 °C) and are expected to be applied to lunar exploration, which has become increasingly active in recent years. Since a ground developm...

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Aerospace - ISSN 2226-4310