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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
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Articles (87)

  • Article
  • Open Access
2 Citations
1,809 Views
27 Pages

Experimental Thermohydraulic Assessment of Novel Curved Ribs for Heat Exchanger Tubes: A Machine Learning Approach

  • Prashant Deshmukh,
  • Subhash Lahane,
  • Hari Sumant,
  • Abhishek D. Patange and
  • Sakthivel Gnanasekaran

Heat transfer enhancement using curved ribs of different cross sections, viz., square, rectangular, triangular, and circular, is a crucial study for designing heat-exchanging devices for various applications, and their thermohydraulic performance pre...

  • Article
  • Open Access
4 Citations
2,585 Views
10 Pages

Measurement and Uncertainty Analysis of Lunar Soil Water Content via Heating Flux Method

  • Ziheng Liu,
  • Huaiyu He,
  • Jiannan Li,
  • Jialong Hao,
  • Junyue Tang,
  • Zhiheng Zhang,
  • Shengyuan Jiang,
  • Guanxin Chi,
  • Ranran Liu and
  • Lei Wang
  • + 2 authors

According to the big impact hypothesis, the moon should be very dry. However, more and more evidence from the remote sensing of the moon in recent years indicates that there is a lot of water in the moon’s polar regions. Researching the source...

  • Article
  • Open Access
2,233 Views
20 Pages

To improve the flame propagation, combustion stability, and uniformity of the temperature field, multi-position injection is applied in a dual-mode combustor by controlling heat release in different locations. Using the chemical reaction of the finit...

  • Article
  • Open Access
2 Citations
1,926 Views
17 Pages

In aero-engines, a secondary air system is used to cool the rotor discs and seal cavities between rotor and stator parts. The pressure loss caused by bleed air can be effectively reduced by setting the finned vortex reducer. Thus, the bleed system de...

  • Article
  • Open Access
3 Citations
1,926 Views
24 Pages

An Online Generation Method of Terminal-Area Trajectories for Wave-Rider Using Deep Neural Networks

  • Zhe Liu,
  • Jie Yan,
  • Bangcheng Ai,
  • Yonghua Fan,
  • Kai Luo,
  • Guodong Cai and
  • Jiankai Qin

This paper presents a deep neural network-based online trajectory generation method for the aerodynamic characteristic description and terminal-area energy management of wave-rider aircrafts. First, the flight dynamics equations in the energy domain...

  • Review
  • Open Access
25 Citations
9,415 Views
31 Pages

Heavily resource-reliant transportation and harsh living conditions, where humans cannot survive without a proper habitat, have prevented humans from establishing colonies on the Moon and Mars. Due to the absence of an atmosphere, potential habitats...

  • Article
  • Open Access
2 Citations
3,160 Views
16 Pages

This paper proposes a trajectory optimization approach for multi-sensor multi-target search and tracking using bearing-only sensors. Based on the framework of the joint integrated probabilistic data association (JIPDA) filter, the intensity of potent...

  • Article
  • Open Access
11 Citations
5,822 Views
26 Pages

Potential Propulsive and Aerodynamic Benefits of a New Aircraft Concept: A Low-Speed Experimental Study

  • Pedro D. Bravo-Mosquera,
  • Hernán D. Cerón-Muñoz and
  • Fernando M. Catalano

The aerodynamic design of a new aircraft concept was investigated through subsonic wind-tunnel testing using 1:28-scale powered models. The aircraft configuration integrates a box-wing layout with engines located at the rear part of the fuselage. Mea...

  • Article
  • Open Access
2 Citations
2,554 Views
18 Pages

An airfoil shape parameterization that can generate a compact design space is highly desirable in practice. In this paper, a compact airfoil parameterization is proposed by incorporating deep learning into the PAERO parameterization method based on t...

  • Article
  • Open Access
2 Citations
2,184 Views
24 Pages

A submerged inlet has good stealth characteristics and a low external drag, but it also has the disadvantage of low internal flow efficiency. In view of this, a new efficiency enhancement method based on the prepositive synergistic bulge of the inlet...

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Aerospace - ISSN 2226-4310