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Aerospace, Volume 7, Issue 8

August 2020 - 17 articles

Cover Story: The inductive pulsed plasma thruster (IPPT) represents a promising and scalable technology for electric propulsion that could be extremely useful in the mission planning trade space due to a demonstrated ability to achieve high efficiency over a range of specific impulse values and to operate over a wide input power range. An IPPT pulses high current through an inductor, producing an electromagnetic field that drives current in a plasma, expelling it at high speed. The IPPT is electrodeless, eliminating electrode erosion found in other electric thrusters and making operation possible in a wide range of propellants. View this paper
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Articles (17)

  • Feature Paper
  • Article
  • Open Access
23 Citations
6,941 Views
25 Pages

Aerostructural Design Exploration of a Wing in Transonic Flow

  • Nicolas P. Bons and
  • Joaquim R. R. A. Martins

14 August 2020

Multidisciplinary design optimization (MDO) has been previously applied to aerostructural wing design problems with great success. Most previous applications involve fine-tuning a well-designed aircraft wing. In this work, we broaden the scope of the...

  • Article
  • Open Access
13 Citations
5,774 Views
26 Pages

Identification of Fixed-Wing Micro Aerial Vehicle Aerodynamic Derivatives from Dynamic Water Tunnel Tests

  • Krzysztof Sibilski,
  • Mirosław Nowakowski,
  • Dariusz Rykaczewski,
  • Paweł Szczepaniak,
  • Andrzej Żyluk,
  • Anna Sibilska-Mroziewicz,
  • Michał Garbowski and
  • Wiesław Wróblewski

13 August 2020

A micro air vehicle (MAV) is a class of miniature unmanned aerial vehicles that has a size restriction and may be autonomous. Fixed-wing MAVs are very attractive for outdoor surveillance missions since they generally offer better payload and enduranc...

  • Article
  • Open Access
95 Citations
14,106 Views
19 Pages

The modern National Airspace System (NAS) is an extremely safe system and the aviation industry has experienced a steady decrease in fatalities over the years. This is in part due the airlines, manufacturers, FAA, and research institutions all contin...

  • Technical Note
  • Open Access
7 Citations
8,275 Views
10 Pages

A new ignition system, based on a CH4/O2 torch has been developed by the Chemical Propulsion Laboratory of the University of Brasilia. Designed to ignite a hybrid rocket, this device has been improved to be used in testing of solid and liquid ramjet...

  • Article
  • Open Access
17 Citations
4,636 Views
18 Pages

Designing a reconfiguration system for an aircraft requires a good mathematical model of the object. An accurate model describing the aircraft dynamics can be obtained from system identification. In this case, special maneuvers for parameter estimati...

  • Article
  • Open Access
12 Citations
9,412 Views
24 Pages

A strong interest in highly-efficient, small-scale propeller configurations can be recognized, especially due to the currently growing number of and usage possibilities for unmanned aerial vehicles (UAVs). Although a variety of different propulsion c...

  • Article
  • Open Access
2 Citations
3,489 Views
15 Pages

In this note, the application of a plant model-based fault detection method for nonlinear control systems on aircraft takeoff is introduced. This method utilizes non-deterministic finite-state automata, which approximate the fault-free dynamics of th...

  • Article
  • Open Access
5 Citations
5,100 Views
14 Pages

Numerical/Experimental Validation of Thin-Walled Composite Box Beam Optimal Design

  • Enrico Cestino,
  • Giacomo Frulla,
  • Paolo Piana and
  • Renzo Duella

Thin-walled composite box beam structural configuration is representative of a specific high aspect ratio wing structure. The optimal design procedure and lay-up definition including appropriate coupling necessary for aerospace applications has been...

  • Article
  • Open Access
13 Citations
4,826 Views
21 Pages

Dynamic Lifecycle Cost Modeling for Adaptable Design Optimization of Additively Remanufactured Aeroengine Components

  • Lydia Lawand,
  • Massimo Panarotto,
  • Petter Andersson,
  • Ola Isaksson and
  • Michael Kokkolaras

Additive manufacturing (AM) is being used increasingly for repair and remanufacturing of aeroengine components. This enables the consideration of a design margin approach to satisfy changing requirements, in which component lifespan can be optimized...

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Aerospace - ISSN 2226-4310