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Aerospace, Volume 13, Issue 1

2026 January - 110 articles

Cover Story: Advances in additive manufacturing are enabling a new generation of aerospike engines, and Pangea Propulsion’s Demo P1 demonstrator showcases how these innovations can overcome long-standing cooling and manufacturability challenges. Building on this progress, our study evaluates the altitude-adaptive behaviour of the truncated aerospike geometry through CFD simulations and introduces a simplified method to estimate its upper bound on base thrust performance, supporting the wider resurgence of aerospike propulsion. View this paper
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Articles (110)

  • Article
  • Open Access
298 Views
22 Pages

Data-Driven Predictive Maintenance for Aircraft Components Through Sparse Event Logs

  • Fulin Sezenoğlu Çetin,
  • Ufuk Üngör,
  • Emre Koyuncu and
  • İbrahim Özkol

22 January 2026

Effective predictive maintenance is crucial for ensuring aircraft reliability, reducing operational disruptions, and supporting spare part inventory management in airline operations. However, maintenance data is often sparse, with irregular observati...

  • Article
  • Open Access
222 Views
19 Pages

22 January 2026

Amidst the increasing aerial traffic and road traffic congestion, Urban Air Mobility (UAM) has emerged as a new mode of aerial transport offering less travel time and ease of portability. A critical factor in reducing travel time is the emerging elec...

  • Article
  • Open Access
181 Views
45 Pages

22 January 2026

Efficient resource allocation is critical for transportation hub operations, yet current scheduling systems require substantial domain-specific customization when deployed across different facilities. This paper presents a domain-adaptive deep reinfo...

  • Article
  • Open Access
132 Views
16 Pages

Dynamic Analysis of the Rod-Traction System for Ship-Borne Aircraft Under High Sea States

  • Guofang Nan,
  • Chen Zhang,
  • Bodong Zhang,
  • Sirui Yang and
  • Jinrui Hu

22 January 2026

The transfer of aircraft on deck relies on the traction system, which is easily affected by the offshore environment. Violent ship motion in the complex marine environment poses a great threat to the aircraft traction process, such as the tire sidesl...

  • Article
  • Open Access
175 Views
15 Pages

High-Energy Detonation Based Lunar Regolith Simulation for Resource Utilization

  • Junyue Tang,
  • Antong Zhao,
  • Shengyuan Jiang,
  • Yang Li,
  • Yu Li,
  • Yi Yang,
  • Zongquan Deng,
  • Xi Wang,
  • Xiangrun Zhao and
  • Tifei Han

22 January 2026

As international lunar exploration shifts from mainly understanding the Moon to equally prioritizing its utilization, the requirement for highly similar lunar regolith simulants has grown. Current simulants, produced mainly by mechanical crushing and...

  • Article
  • Open Access
172 Views
17 Pages

21 January 2026

Aerospace power systems, including satellites in low earth orbit (LEO) and geostationary earth orbit (GEO), face stringent thermal constraints to minimize size, weight, and power (SWaP). Gallium nitride (GaN) devices offer superior radiation hardness...

  • Review
  • Open Access
335 Views
21 Pages

21 January 2026

Nitrous oxide (N2O) has attracted increasing attention as an oxidizer for space propulsion systems due to its non-toxic nature and favorable handling characteristics. Its relatively high vapor pressure allows self-pressurization, while its wide stora...

  • Article
  • Open Access
237 Views
22 Pages

Unsteady Aerodynamics of Continuously Morphing Airfoils from Transonic to Hypersonic Regimes

  • Linyi Zhi,
  • Renqing Zhai,
  • Yu Yang,
  • Xintong Shi and
  • Zhigang Wang

21 January 2026

Designing high-speed aircraft for wide-speed-range operation remains a major aerodynamic challenge. This study investigates the unsteady aerodynamics of a continuously morphing airfoil from transonic to hypersonic regimes. A smooth morphing trajector...

  • Article
  • Open Access
159 Views
26 Pages

21 January 2026

During lunar landing and takeoff, an extremely under-expanded jet from retrorocket engines generates a complex impingement flow, including multiple shocks and a near-field recirculation bubble, posing critical risks to lunar missions. To clarify the...

  • Article
  • Open Access
151 Views
22 Pages

Cell-Based Optimization of Air Traffic Control Sector Boundaries Using Traffic Complexity

  • César Gómez Arnaldo,
  • José María Arroyo López,
  • Raquel Delgado-Aguilera Jurado,
  • María Zamarreño Suárez,
  • Javier Alberto Pérez Castán and
  • Francisco Pérez Moreno

20 January 2026

The increasing demand for air travel has intensified the need for more efficient air traffic management (ATM) solutions. One of the key challenges in this domain is the optimal sectorization of airspace to ensure balanced controller workload and oper...

  • Article
  • Open Access
172 Views
16 Pages

20 January 2026

The Linked Autonomous Interplanetary Satellite Orbit Navigation (LiAISON) technique enables cislunar spacecraft to obtain accurate position and velocity information, allowing full state estimation of two vehicles using only inter-satellite range (ISR...

  • Article
  • Open Access
208 Views
16 Pages

20 January 2026

Accurately characterizing the structural state of membrane reflector antennas (MRA) remains challenging due to the difficulty in determining stress distribution through geometric measurement alone. Although photogrammetry provides high-precision geom...

  • Article
  • Open Access
190 Views
20 Pages

19 January 2026

Transonic shock buffet is a complex flow phenomenon characterized by self-sustained shock oscillations, which severely limits the flight envelope of modern civil aircraft. While Shock Control Bumps (SCBs) have been widely studied for drag reduction,...

  • Article
  • Open Access
417 Views
27 Pages

Investigating XR Pilot Training Through Gaze Behavior Analysis Using Sensor Technology

  • Aleksandar Knežević,
  • Branimir Krstić,
  • Aleksandar Bukvić,
  • Dalibor Petrović and
  • Boško Rašuo

16 January 2026

This research aims to characterize extended reality flight trainers and to provide a detailed account of the sensors employed to collect data essential for qualitative task performance analysis, with a particular focus on gaze behavior within the ext...

  • Article
  • Open Access
308 Views
25 Pages

15 January 2026

Reducing the sonic boom intensity and increasing the cruise lift-to-drag ratio are pivotal technologies for the successful development of supersonic civil aircraft. To address the limitation that sonic boom research primarily focuses on characteristi...

  • Article
  • Open Access
274 Views
27 Pages

Sustainability-Driven Design Optimization of Aircraft Parts Using Mathematical Modeling

  • Aikaterini Anagnostopoulou,
  • Dimitris Sotiropoulos,
  • Ioannis Sioutis and
  • Konstantinos Tserpes

15 January 2026

The design of aircraft components is a complex process that must simultaneously account for environmental impact, manufacturability, cost and structural performance to meet modern regulatory requirements and sustainability objectives. When these fact...

  • Article
  • Open Access
281 Views
19 Pages

Computational Study of Hybrid Propeller Configurations

  • Mingtai Chen,
  • Tianming Liu,
  • Jack Edwards and
  • Tiegang Fang

15 January 2026

This study presents the first computational investigation of hybrid propeller configurations that combine toroidal and conventional blade geometries. Using Delayed Detached Eddy Simulation (DDES) with the Shear Stress Transport (SST) kω...

  • Article
  • Open Access
179 Views
21 Pages

15 January 2026

Prolonged +Gz acceleration during high-performance flight exposes pilots to the risk of G-induced loss of consciousness (G-LOC), a dangerous condition that compromises operational safety. To enable early detection without intrusive sensors, we presen...

  • Article
  • Open Access
343 Views
22 Pages

15 January 2026

Detailed knowledge regarding the thermophysical properties and electrical conductivity of the combustion products derived from solid propellants is essential for the optimized design and operation of solid-fuel rocket engines employing magnetohydrody...

  • Article
  • Open Access
347 Views
20 Pages

15 January 2026

Compared with conventional symmetric aircraft, the oblique-wing aircraft offers significant advantages across a wide speed range due to the variable oblique angle. However, the asymmetric aerodynamic characteristics will arise from the differential l...

  • Article
  • Open Access
271 Views
24 Pages

14 January 2026

Three-dimensional printing is the most commonly used method for producing customized or mock-up products for industrial applications. In particular, aviation devices for drones usually require a high spatial resolution to satisfy the small size requi...

  • Article
  • Open Access
207 Views
24 Pages

14 January 2026

During the service life of a supersonic aircraft, panels are susceptible to damaged boundary supports and unexpected attached masses, which can critically alter their flutter characteristics. This paper proposes a novel two-stage assumed mode method...

  • Article
  • Open Access
223 Views
15 Pages

14 January 2026

Accurate quantification of aircraft emissions and their uncertainties is essential for well-informed policy-making, air quality management, and the development of sustainable airport strategies. This study addresses uncertainties in aircraft emission...

  • Review
  • Open Access
240 Views
33 Pages

Center of Mass Measurement Technology and Its Research Progress in the Aerospace Field

  • Huan Wang,
  • Qilong Jiang,
  • Hanbin Zhu,
  • Wenke Zhou,
  • Chang Liu and
  • Hongchao Zhao

13 January 2026

The center of mass is a key parameter characterizing the mass distribution of an object, and its measurement holds significant importance in high-tech fields such as aerospace, the defense industry, and precision manufacturing. With modern engineerin...

  • Article
  • Open Access
598 Views
16 Pages

Economic Analysis of a ROXY Pilot Plant Supporting Early Lunar Mission Architectures

  • Tehya F. Birch,
  • Achim Seidel,
  • James E. Johnson,
  • Georg Poehle and
  • Uday Pal

13 January 2026

The establishment of a sustained human presence on the Moon is critically dependent on the ability to utilize local resources, primarily the production of oxygen for life support and propellant. The ROXY (Regolith to Oxygen and metals conversion) pro...

  • Review
  • Open Access
464 Views
22 Pages

13 January 2026

Research into Remotely Piloted Aircraft Systems (RPASs) has expanded rapidly, yet the competencies, knowledge, skills, and other attributes (KSaOs) required of RPAS pilots remain comparatively underexamined. This review consolidates existing studies...

  • Article
  • Open Access
300 Views
24 Pages

13 January 2026

This study systematically investigates the effects of manufacturing errors on the drag reduction performance of micro-grooves fabricated using roll-to-roll hot embossing technology. Numerical simulations were conducted to analyze the drag reduction c...

  • Article
  • Open Access
285 Views
21 Pages

13 January 2026

Cavitation in aircraft hydraulic systems continues to pose a serious problem for the aviation industry. This paper presents a new study on cavitation in aviation hydraulic fluid AMG-10 at its inception condition, corresponding to a relative pressure...

  • Article
  • Open Access
279 Views
36 Pages

12 January 2026

This study presents an integrated optimization framework for fleet assignment, flight scheduling, and aircraft routing under uncertainty, addressing a core challenge in airline operational planning. A three-stage stochastic mixed-integer nonlinear pr...

  • Article
  • Open Access
523 Views
25 Pages

Advanced Sensor Tasking Strategies for Space Object Cataloging

  • Alessandro Mignocchi,
  • Sebastian Samuele Rizzuto,
  • Alessia De Riz and
  • Marco Felice Montaruli

12 January 2026

Space Surveillance and Tracking (SST) plays a crucial role in ensuring space safety. To this end, accurate and numerous observational resources are needed to build and maintain a catalog of space objects. In particular, it is essential to develop opt...

  • Article
  • Open Access
439 Views
25 Pages

12 January 2026

With the cost-saving benefits of reusable launch vehicles (RLVs), South Korea is pursuing the application of reusability technologies to KSLV-III. While SpaceX currently reuses only the first stage of Falcon 9, the Starship program aims for full-stag...

  • Article
  • Open Access
342 Views
27 Pages

12 January 2026

As global airspace operations grow increasingly complex, the risk of near-mid-air collisions (NMACs) poses a persistent and critical challenge to aviation safety. Traditional collision-avoidance systems, while effective in many scenarios, are limited...

  • Article
  • Open Access
409 Views
36 Pages

11 January 2026

The optimization of low-Reynolds-number airfoils for micro unmanned aerial vehicles (UAVs) is challenging due to strong geometric nonlinearities, tight endurance requirements, and the need to maintain performance across multiple operating conditions....

  • Article
  • Open Access
247 Views
19 Pages

11 January 2026

Decision-making for maneuvering in the presence of long-range threats is crucial for enhancing the safety and reliability of autonomous aerial platforms operating in beyond-line-of-sight environments. This study employs the Deep Q-Network (DQN) metho...

  • Article
  • Open Access
357 Views
21 Pages

11 January 2026

Due to the complexity of aerodynamic coupling between the duct and propeller, the overall design and optimization of ducted fans often require extensive experience and time. Meanwhile, traditional design methods based on Blade Element Momentum Theory...

  • Article
  • Open Access
238 Views
24 Pages

10 January 2026

Clearance in joints caused by assemblage, manufacturing errors, and wear is inevitable, which will affect the dynamic performance of the dual-manipulator system on spacecraft. The motion of the dual-manipulator system with clearances in imperfect joi...

  • Article
  • Open Access
326 Views
22 Pages

An FPGA+DSP-Based On-Orbit Software Updating Architecture and Strategy for Satellite Payload Control Systems

  • Peijun Zhong,
  • Chongru Wang,
  • Maoxing Wen,
  • Hongsong Qu,
  • Yueming Wang and
  • Tao Wang

10 January 2026

This paper presents an architecture and strategy for on-orbit software updating of satellite payload control systems, based on a tightly coupled DSP and FPGA design. The architecture achieves tight coupling between the DSP and FPGA via the XINTF inte...

  • Article
  • Open Access
319 Views
17 Pages

Decision Tree-Based Pilot Workload Prediction Through Optimized HRV Features Selection

  • Carmelo Rosario Vindigni,
  • Giuseppe Iacolino,
  • Antonio Esposito,
  • Calogero Orlando and
  • Andrea Alaimo

This research explores the use of physiological signals derived from heart activity to assess mental effort during flight-related tasks. Data were collected through wearable sensors during simulations with varying cognitive demands. Specific indicato...

  • Article
  • Open Access
263 Views
21 Pages

Convergence rate is a key performance index for flight vehicles, and accelerating it remains a critical open issue. In this paper, a fast robust integrated guidance and control scheme for flight vehicles based on convergence rate estimation mechanism...

  • Article
  • Open Access
288 Views
19 Pages

Civil airplanes encounter unpredictable safety risks due to uncertain environmental disturbances, mechanical failures, and pilot mis-operations. This paper develops a virtual flight method (VFM) consisting of a series of techniques including flight m...

  • Article
  • Open Access
505 Views
25 Pages

A Comparative Study of Liquid Film Cooling on a Flat Plate Using SPH and VOF Methods

  • Edidiong Michael Umana,
  • Huan Li,
  • Xiufeng Yang,
  • Dmitry Alexandrovich Uglanov and
  • Naresh Kedam

This numerical study demonstrates the existence of a critical injection momentum threshold necessary for stable liquid film formation, highlighting that either excessive or insufficient momentum degrades cooling performance. This optimization is crit...

  • Article
  • Open Access
334 Views
23 Pages

This study employed numerical simulations to investigate the aerodynamic characteristics of a flapping wing by solving the governing incompressible Navier–Stokes equations. Using computational fluid dynamics (CFD), the effect of frequency accel...

  • Article
  • Open Access
298 Views
25 Pages

Online Synchronous Coordinated Assignment and Planning for Heterogeneous Fixed-Wing UAVs

  • Xindi Wang,
  • Jiansong Zhang,
  • Zhenyu Ma,
  • Chuanshuo Cao and
  • Hao Liu

This paper addresses the Multi-Target Reconnaissance (MTR) problem for heterogeneous Fixed-Wing Unmanned Aerial Vehicles (FW-UAVs), focusing on synchronized and time-optimal mission execution under stringent constraints. A two-stage coordinated assig...

  • Article
  • Open Access
266 Views
28 Pages

Utilizing coordinated UAV formations for emergency disaster relief is a key future trend, but traditional evaluation methods have three major drawbacks: high computational complexity, heavy reliance on expert experience, and poor generalization in mu...

  • Article
  • Open Access
1 Citations
340 Views
30 Pages

Feasibility Analysis of a Return to Launch Site Partially Reusable Microlauncher via Multidisciplinary Optimization

  • Alexandru-Iulian Onel,
  • Tudorel-Petronel Afilipoae,
  • Oana-Iuliana Popescu,
  • Georgiana Ichim,
  • Alexandra Popescu and
  • Ionuț Bunescu

Reusable launch vehicles are a key category of next-gen European launchers, as multiple companies are in advanced stages of study and are shifting towards the development of first demonstrators. A worldwide tendency to reduce the costs associated wit...

  • Article
  • Open Access
244 Views
16 Pages

Microvibration Suppression for the Survey Camera of CSST

  • Renkui Jiang,
  • Wei Liang,
  • Libin Wang,
  • Enhai Liu,
  • Xuerui Liu,
  • Yongchao Zhang,
  • Sixian Le,
  • Zhaoyang Li,
  • Hongyu Wang and
  • Ang Zhang
  • + 7 authors

The Survey Camera (SC) is the key instrument of the China Space Station Telescope (CSST), with its imaging performance significantly constrained by microvibrations from internal sources such as the shutter and cryocoolers. This paper proposes a syste...

  • Article
  • Open Access
289 Views
25 Pages

Effect of Nose Bluntness on Boundary-Layer Transition of a Fin–Cone Configuration at Mach 6

  • Ziyan Fang,
  • Lang Xu,
  • Duolong Xu,
  • Xueliang Li,
  • Fu Zhang and
  • Jie Wu

Experiments on hypersonic boundary-layer instability of a fin–cone configuration were conducted in a Φ 0.5 m Mach 6 Ludwieg tube tunnel. Infrared thermography and high-frequency pressure sensors were used to measure the transition front and...

  • Article
  • Open Access
297 Views
13 Pages

Experimental Study of a Planar Solid-Propellant Pulsed Plasma Thruster Using Graphite

  • Merlan Dosbolayev,
  • Zhanbolat Igibayev and
  • Ongdassyn Yertayev

The study presents an upgraded design and the results of experimental investigations of a solid-propellant pulsed plasma thruster (PPT) in which graphite simultaneously serves as both the propellant and the ignition element. The proposed configuratio...

  • Article
  • Open Access
476 Views
16 Pages

Automated detection of impact craters is essential for planetary surface studies, yet it remains a challenging task due to variable morphology, degraded rims, complex geological settings, and inconsistent illumination conditions. This study presents...

  • Article
  • Open Access
333 Views
80 Pages

This research investigates the process of determining and maintaining the Acceptable Level of Safety Performance (ALoSP) at an airport, utilizing a case study conducted at Split Airport. The study illustrates how the ALoSP framework, originally devel...

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Aerospace - ISSN 2226-4310