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Aerospace, Volume 12, Issue 10

October 2025 - 90 articles

Cover Story: While high-performance chemical in-space propulsion has been dominated by nitrogen-tetroxide-based oxidizers and hydrazine derivatives as fuel, next-generation systems may benefit from green technologies. One of the candidate oxidizers is 98% Hydrogen Peroxide. While historically High-Test Peroxide (HTP) was utilized at concentrations up to 90%, novel solutions focus on 98% HTP. Pulse mode and steady-state operations have been demonstrated using both hypergolic fuels and quasi-hypergolic ignition, which is possible thanks to modern catalyst beds for 98% HTP. Deep-throttleable systems are feasible. There are continued development efforts regarding long-term storability, and the recent advances provide prospects for reducing costs without sacrificing performance, unlike with lower HTP grades. View this paper
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Articles (90)

  • Article
  • Open Access
729 Views
22 Pages

Fire Control Radar Fault Prediction with Real-Flight Data

  • Minyoung Kim,
  • Ikgyu Lee,
  • Seon-Ho Jeong,
  • Dawn An and
  • Byoungserb Shim

21 October 2025

Unexpected failures of avionics equipment critically affect flight safety, operational availability, and maintenance costs. To address these issues, Condition-Based Maintenance Plus (CBM+) has emerged as a strategy to optimize maintenance timing base...

  • Article
  • Open Access
411 Views
23 Pages

21 October 2025

The discrete-serpentine heterogeneous multi-arm space robot (DSHMASR) has more advantages than single discrete space robots or single serpentine space robots in complex tasks of on-orbit servicing. However, the mechanical structure complexity of the...

  • Article
  • Open Access
650 Views
21 Pages

21 October 2025

Space robots are vital for in-orbit maintenance of large satellites, but dense payloads and complex surface structures pose challenges for safe crawling operations. This study proposes an improved trajectory planning framework for three-dimensional s...

  • Article
  • Open Access
547 Views
32 Pages

19 October 2025

The unprecedented increase in the number of objects orbiting the Earth necessitates a comprehensive characterisation of these objects to improve the effectiveness of Space Surveillance and Tracking (SST) operations. In particular, accurate knowledge...

  • Article
  • Open Access
406 Views
14 Pages

19 October 2025

The design of spacecraft protection against orbital debris (OD) is generally based on experiments and models involving spherical projectiles. However, observations of collision fragments from ground-based satellite impact experiments have shown that...

  • Article
  • Open Access
525 Views
18 Pages

18 October 2025

Coaxial co-rotating (CCR) propeller systems provide structural simplicity, compactness, and high disk loading, making them attractive for an Electric Distributed Propulsion System (EDPS). However, aerodynamic interactions between the upper and lower...

  • Article
  • Open Access
495 Views
20 Pages

17 October 2025

This paper addresses the critical multiple-uncertainty challenge in laser link acquisition for space gravitational wave detection missions—a key bottleneck where spacecraft attitude alignment for laser link establishment is perturbed by inheren...

  • Article
  • Open Access
478 Views
20 Pages

17 October 2025

In this paper, a finite-time three-axis stabilization controller for an underactuated rigid spacecraft is proposed based on well-designed hierarchical terminal sliding mode surfaces to handle the insufficiency of control effort and disturbances. Firs...

  • Article
  • Open Access
626 Views
29 Pages

17 October 2025

A ram air turbine serves as a critical emergency power system for aircraft. To mitigate aerodynamic losses from tip vortices, this study proposes three blade tip enhancement configurations: a tip plate, tip contraction, and winglet. Numerical results...

  • Article
  • Open Access
362 Views
15 Pages

17 October 2025

Virtual commands serve as the essential framework for establishing interaction between the virtual pilot and the MCP in autopilot scenarios. Conventional proportional-integral-derivative (PID) controllers are insufficient to ensure accurate flight tr...

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Aerospace - ISSN 2226-4310