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Aerospace, Volume 7, Issue 2

February 2020 - 10 articles

Cover Story: Scheme of the thermally controlled iodine feeding system developed at Università di Pisa and its calibration curve of the generated mass flow rate, showing both experimental and numerical results. On the bottom right, a picture of the evolution of the feeding system concept, including a flexible heated pipe between the tank and the thermal throttle to improve the coupling with the thruster during the propulsion system’s experimental campaign. View this paper.
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Articles (10)

  • Article
  • Open Access
14 Citations
7,181 Views
20 Pages

25 February 2020

Nanosatellites are increasingly being used in space-related applications to demonstrate and test scientific capability and engineering ingenuity of space-borne instruments and for educational purposes due to their favourable low manufacturing costs,...

  • Article
  • Open Access
26 Citations
14,014 Views
15 Pages

24 February 2020

CubeSats usually adopt aluminum alloys for primary structures, and a number of studies exist on Carbon Fiber Reinforced Plastic (CFRP) primary structures. The internal volume of a spacecraft is usually occupied by battery arrays, reducing the volume...

  • Article
  • Open Access
7 Citations
6,317 Views
21 Pages

Effect of Hot-Wet Storage Aging on Mechanical Response of a Woven Thermoplastic Composite

  • Theofanis S. Plagianakos,
  • Kirsa Muñoz,
  • Diego Saenz-Castillo,
  • Maria Mora Mendias,
  • Miguel Jiménez and
  • Vasileios Prentzias

24 February 2020

The effect of hot-wet storage aging on the mechanical response of a carbon fiber polyether ether ketone (PEEK)-matrix woven composite has been studied. A wide range of static loads and selected cyclic load tests on the interlaminar fatigue strength w...

  • Article
  • Open Access
16 Citations
9,219 Views
14 Pages

21 February 2020

The decision of a flight crew to undertake a go-around, aborting a landing attempt, is primarily to ensure the safe conduct of a flight. Although go-arounds are rare, they do cause air traffic disruption, especially in busy airspace, due to the need...

  • Article
  • Open Access
4 Citations
6,837 Views
26 Pages

20 February 2020

Current Air Traffic Controller working positions (CWPs) are reaching their capacity owing to increasing levels of air traffic. The multimodal CWP prototype TriControl combines automatic speech recognition, multitouch gestures, and eye-tracking, aimin...

  • Article
  • Open Access
16 Citations
8,302 Views
20 Pages

9 February 2020

Nowadays, technologies have a massive impact on the design of avionic systems, even for the conservative space industry. In this paper, the single event effect (SEE) characterization of a highly integrated and radio frequency (RF) agile transceiver i...

  • Article
  • Open Access
8 Citations
5,279 Views
11 Pages

6 February 2020

Further investigation on the impact of the so called Peukert effect on optimal control of a battery-electrically driven airplane is presented. To analyse the impact of the Peukert effect, an ideal model without this battery concerning effect and a re...

  • Article
  • Open Access
17 Citations
5,954 Views
15 Pages

Mitigation and Predictive Assessment of SET Immunity of Digital Logic Circuits for Space Missions

  • Ygor Q. Aguiar,
  • Frédéric Wrobel,
  • Jean-Luc Autran,
  • Paul Leroux,
  • Frédéric Saigné,
  • Vincent Pouget and
  • Antoine D. Touboul

5 February 2020

Due to the intrinsic masking effects of combinational circuits in digital designs, Single-Event Transient (SET) effects were considered irrelevant compared to the data rupture caused by Single-Event Upset (SEU) effects. However, the importance of con...

  • Technical Note
  • Open Access
6 Citations
5,772 Views
11 Pages

Remote and Feedback Control of the Flap Angle in a Wind Tunnel Test Model by Optical Measurement

  • Kazuhisa Chiba,
  • Tatsuro Komatsu,
  • Hiroyuki Kato and
  • Kazuyuki Nakakita

31 January 2020

We have developed a remote and precise feedback control system using optical measurement technology to alter the angle of a flap, which is part of a wind tunnel test model, automatically and to earn the aerodynamic data efficiently. To rectify the wa...

  • Article
  • Open Access
12 Citations
7,310 Views
18 Pages

Modeling and Characterization of a Thermally Controlled Iodine Feeding System for Electric Propulsion Applications

  • Manuel Martín Saravia,
  • Luca Bernazzani,
  • Alessio Ceccarini,
  • Alfio Emanuele Vinci and
  • Fabrizio Paganucci

23 January 2020

Iodine is considered as a feasible alternative to xenon as a propellant for electric propulsion systems, thanks to its good propulsive performance, high availability, and high storage density. However, as iodine is stored in solid state at ambient te...

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Aerospace - ISSN 2226-4310