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Aerospace, Volume 12, Issue 2

February 2025 - 90 articles

Cover Story: This study explores a mission concept for a recoverable LEO satellite carrying a scientific payload, through the comparison between one using an aero-brake heat shield without propulsion assistance and another with the same system but supported by a thruster. Aerodynamic analysis via DSMC assessed drag and stability. A ∆V of ~100 m/s cut descent time from 54 days to under 1 h, maintaining trajectory. Drag uncertainties caused ~100 km dispersion, while a ±1% impulse error increased it to 400 km. A 4 kg monopropellant thruster was designed within a 250 mm high and 350 mm diameter casing, supporting three layout options. View this paper
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Articles (90)

  • Article
  • Open Access
1,261 Views
24 Pages

Ascent Trajectory Optimization Using Second-Order Birkhoff Pseudospectral Methods

  • Xiaopeng Xue,
  • Yujia Xie,
  • Hui Zhou,
  • Qinghai Gong and
  • Dangjun Zhao

13 February 2025

This paper proposes a novel convex optimization framework for two-stage launch vehicle (TSLV) ascent trajectory planning from liftoff to orbit insertion, featuring two groundbreaking advancements over existing convex optimization methodologies: (1) a...

  • Article
  • Open Access
1 Citations
2,610 Views
27 Pages

13 February 2025

This paper investigates and evaluates the accuracy of various empirical and semi-empirical methods for predicting aircraft wing-structure mass. Eight methods were selected and analysed using data from large passenger-transport aircraft. The required...

  • Article
  • Open Access
2 Citations
1,597 Views
24 Pages

13 February 2025

Adhesively bonded joints are essential in the aeronautical industry, offering benefits such as weight reduction and enhanced sustainability. However, certifying these joints is challenging due to unreliable methods for assessing their strength and th...

  • Article
  • Open Access
3 Citations
2,122 Views
27 Pages

13 February 2025

Eco-design is an innovative design methodology that focuses on minimizing the environmental footprint of industries, including aviation, right from the conceptual and development stages. However, rising industrial demand calls for a more comprehensiv...

  • Article
  • Open Access
2 Citations
1,200 Views
28 Pages

12 February 2025

An asymptotic analytical method is proposed to study the thermal post-buckling behaviors of fiber-reinforced composite (FRC)-laminated beams with geometric imperfections employing a modified zig-zag beam model. The beam model satisfied the discontinu...

  • Article
  • Open Access
1 Citations
3,518 Views
27 Pages

12 February 2025

Delays are a global issue affecting both airports and airlines. Departure delays are particularly likely to propagate across airports, rendering the entire flight network susceptible to increased delay durations. The delay network and its duration fl...

  • Article
  • Open Access
2,650 Views
33 Pages

Evaluation and Performance Optimization of a Hydrogen Peroxide-Based Green Monopropellant Thruster for Steady-State Operations

  • Uğur Kokal,
  • Mustafa Baysal,
  • Nur Ber Emerce,
  • Yiğit Yıldız,
  • Arif Karabeyoğlu and
  • İbrahim Özkol

12 February 2025

Hydrogen peroxide (High Test Peroxide, HTP) emerges as a promising candidate for green space propulsion applications due to its lower toxicity compared to liquid conventional propellants such as hydrazine and nitrogen tetroxide. This study aims to op...

  • Article
  • Open Access
8 Citations
1,089 Views
20 Pages

Dynamics Modeling and Analysis of Rotating Trapezoidal Flexible Plate System with Large Deformation

  • Yongbin Guo,
  • Xian Guo,
  • Ming Li,
  • Jing Zhang,
  • Dingguo Zhang and
  • Jiajun Wu

11 February 2025

Origami-derived space-deployable structures have a broad application prospect in the aerospace field owing to their excellent morphology transformation performance, and they are usually large-scale and lightweight. However, their deformation increase...

  • Article
  • Open Access
1 Citations
2,691 Views
21 Pages

10 February 2025

This paper investigates the problem of angular momentum control and planning for control moment gyroscope(CMG) arrays in rigid spacecraft attitude control systems using deep reinforcement learning (DRL). Specifically, a DRL-based angular momentum con...

  • Article
  • Open Access
1,227 Views
32 Pages

10 February 2025

Due to irregular hydrodynamic–aerodynamic coupling, the modeling and simulation of near-surface flight are extremely complex. For the present study, a practical dynamic model and a complete motion simulation method for the solution of such prob...

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Aerospace - ISSN 2226-4310