You are currently viewing a new version of our website. To view the old version click .

Aerospace, Volume 10, Issue 7

July 2023 - 87 articles

Cover Story: Hybrid rocket engines (HREs) offer a low-cost, reliable, and environmentally friendly solution for both launch and in-space applications. Hybrid propellants have been identified as green, thanks to their use of non-toxic, non-carcinogenic oxidizers. Of particular relevance are storable oxidizers, namely high-concentration (≥90 wt.%) hydrogen peroxide (HP, H2O2) and nitrous oxide (N2O). This work provides a survey of experimental activities based on H2O2 and N2O for hybrid rocket propulsion applications, focusing on lab-scale activities and sounding rockets. Open literature data are provided with original thermochemical calculations to support the discussion. View this paper
  • Issues are regarded as officially published after their release is announced to the table of contents alert mailing list .
  • You may sign up for email alerts to receive table of contents of newly released issues.
  • PDF is the official format for papers published in both, html and pdf forms. To view the papers in pdf format, click on the "PDF Full-text" link, and use the free Adobe Reader to open them.

Articles (87)

  • Article
  • Open Access
3 Citations
3,184 Views
13 Pages

Wildlife strikes in aviation represent a serious economic concern; however, in some jurisdictions, the costs associated with this phenomenon are not collected or shared. This hampers the industry’s ability to quantify the risk and assess the po...

  • Article
  • Open Access
5 Citations
5,561 Views
18 Pages

A Novel Composite Helicopter Tail Rotor Blade with Enhanced Mechanical Properties

  • Anton Hadăr,
  • Andrei-Daniel Voicu,
  • Florin Baciu,
  • Daniel Vlăsceanu,
  • Daniela-Ioana Tudose and
  • Ştefan-Dan Pastramă

This paper describes the transition towards a composite structure, with the same overall aerodynamic characteristics, for a tail rotor blade of an IAR330 helicopter. The newly proposed structure of the composite blade is made of a carbon-roving spar...

  • Article
  • Open Access
3 Citations
2,264 Views
21 Pages

Obvious aeroelastic deformation occurs in spinning projectiles with large slenderness ratio, which seriously affects flight stability and maneuverability. This paper investigates the aeroelastic response of spinning projectiles with large slenderness...

  • Article
  • Open Access
4 Citations
2,322 Views
15 Pages

Traditional methods are unable to effectively assess the health status of engine bleed air systems. To address the limitation, this paper proposes a methodology for constructing health indicators using multi-level feature extraction. First, this appr...

  • Article
  • Open Access
16 Citations
4,768 Views
24 Pages

Sensor health assessments are of great importance for accurately understanding the health of an aeroengine, supporting maintenance decisions, and ensuring flight safety. This study proposes an intelligent framework based on a physically guided neural...

  • Review
  • Open Access
16 Citations
20,217 Views
22 Pages

Hybrid rockets using specific oxidizer–fuel combinations are considered a green alternative to current propulsion systems, as they do not release very toxic or polluting exhausts, but only much less harmful substances such as carbon monoxide/di...

  • Article
  • Open Access
5 Citations
2,450 Views
21 Pages

The penetration of unmanned aerial vehicles (UAVs) is an important aspect of UAV games. In recent years, UAV penetration has generally been solved using artificial intelligence methods such as reinforcement learning. However, the high sample demand o...

  • Article
  • Open Access
3 Citations
2,640 Views
38 Pages

In an axial-flow turbine of a jet engine used for aircraft propulsion, the passage vortex (PV) and tip leakage vortex (TLV) generated inside the blade passage deteriorate the aerodynamic performance. In this study, a dielectric barrier discharge plas...

  • Article
  • Open Access
5 Citations
3,473 Views
24 Pages

High-Precision Magnetic Testbed Design and Simulation for LEO Small-Satellite Control Test

  • Jhonny Uscategui,
  • Xinsheng Wang,
  • Gerson Cuba and
  • María Guarirapa

Small satellites with academic missions in low Earth orbit (LEO) employ magnetic attitude control systems primarily due to their ease of development and low cost. These systems utilize magnetorquers to generate a magnetic moment that interacts with E...

  • Article
  • Open Access
7 Citations
4,101 Views
21 Pages

In recent years, artificial intelligence (AI) technology has been applied in different research fields. In this study, the XGBoost regression model is proposed to estimate JT9D engine thrust. The model performance mean absolute error (MAE) is 0.00484...

of 9

Get Alerted

Add your email address to receive forthcoming issues of this journal.

XFacebookLinkedIn
Aerospace - ISSN 2226-4310