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Aerospace, Volume 9, Issue 7

July 2022 - 63 articles

Cover Story: Venusian clouds are conjectured to be a possible habitat for life. We propose a mission to explore the clouds of Venus to evaluate their habitability and to search for signs of life. The spacecraft would launch from Earth with an orbiter and a probe carrying an aerobot. A super-pressure balloon would cycle at altitudes between 48 and 60 km using a combination of ballast drop, gas venting, and the thermal effects of the environment. The gondola design is derived from the Pioneer Venus Large Probe pressure vessel. The aerobot would transmit data via orbiter relay combined with a direct-to-Earth link. The proposed mission could help to elucidate the limits of habitability and the role of unknown chemistry or the possibly life itself in the atmosphere of Venus. View this paper
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Articles (63)

  • Article
  • Open Access
3 Citations
2,524 Views
19 Pages

The velocity and acceleration of geostationary transfer orbit (GTO) satellites change dramatically and periodically, and the operating area extends from hundreds of kilometers to 36,000 km above the Earth’s surface. This leads to the limitation...

  • Article
  • Open Access
10 Citations
6,093 Views
24 Pages

Trajectory optimization has been an active area of research for air transport studies for several decades. But almost all flight optimizers proposed in the literature remain close-sourced, which presents a major disadvantage for the advancement of sc...

  • Article
  • Open Access
2 Citations
2,442 Views
24 Pages

Shape Optimisation of Assembled Plate Structures with the Boundary Element Method

  • Llewellyn Morse,
  • Vincenzo Mallardo,
  • Zahra Sharif-Khodaei and
  • Ferri M.H. Aliabadi

A novel methodology is presented for performing sensitivity analyses of assembled plate structures using the Boundary Element Method (BEM). The main novelty of this work is that the exact implicit derivatives of the BEM formulations for assembled pla...

  • Article
  • Open Access
24 Citations
9,045 Views
18 Pages

Design and Analysis of MataMorph-3: A Fully Morphing UAV with Camber-Morphing Wings and Tail Stabilizers

  • Peter L. Bishay,
  • James S. Kok,
  • Luis J. Ferrusquilla,
  • Brian M. Espinoza,
  • Andrew Heness,
  • Antonio Buendia,
  • Sevada Zadoorian,
  • Paul Lacson,
  • Jonathan D. Ortiz and
  • Ruiki Basilio
  • + 1 author

Conventional aircraft use discrete flight control surfaces to maneuver during flight. The gaps and discontinuities of these control surfaces generate drag, which degrades aerodynamic and power efficiencies. Morphing technology aims to replace convent...

  • Article
  • Open Access
10 Citations
5,026 Views
17 Pages

Conceptual Research on a Mono-Biplane Aerodynamics-Driven Morphing Aircraft

  • Tingyu Guo,
  • Liangtao Feng,
  • Chenhua Zhu,
  • Xiaopeng Zhou and
  • Haixin Chen

The operation of aircrafts with high aspect ratio wings is usually vulnerable to low-standard airports and bad weather. A new concept for a mono-biplane aerodynamics-driven morphing aircraft is proposed. The movable and fixed wings form a biplane mod...

  • Article
  • Open Access
6 Citations
4,840 Views
15 Pages

Flow Feature in Supersonic Non-Isobaric Jet near the Nozzle Edge

  • Valeriy Zapryagaev,
  • Ivan Kavun and
  • Nikolay Kiselev

Using the example of studying the supersonic underexpanded jet initial section, the issue of interpreting the experimental visualization data and Pitot pressure measurement data using the results of numerical calculations (2d RANS k-ω SST) is d...

  • Article
  • Open Access
6 Citations
3,812 Views
30 Pages

A coupled aerostructural aircraft design and trajectory optimization framework is developed for the Air Cargo Challenge competition to maximize the expected score based on cargo carried, altitude achieved and distance traveled. Its modular architectu...

  • Article
  • Open Access
8 Citations
3,534 Views
17 Pages

This work addresses the problem of vertical wind profile online estimation at a given location. Specifically, the north and east components of the wind are continuously estimated as functions of time and altitude at two waypoints used for landing on...

  • Article
  • Open Access
3,406 Views
24 Pages

The Stability Analysis of a Tether for a Segmented Space Elevator

  • Shihao Luo,
  • Naigang Cui,
  • Xiaowei Wang,
  • Youhua Fan and
  • Haitao Gu

The space elevator system is a space tether system used to solve low-cost space transportation. Its high efficiency, large load and other characteristics have broad application prospects in the aerospace field. The stability analysis is the foundatio...

  • Communication
  • Open Access
16 Citations
5,545 Views
17 Pages

Design Principles for a Contrail-Minimizing Trial in the North Atlantic

  • Jarlath Molloy,
  • Roger Teoh,
  • Seán Harty,
  • George Koudis,
  • Ulrich Schumann,
  • Ian Poll and
  • Marc E. J. Stettler

The aviation industry has committed to decarbonize its CO2 emissions. However, there has been much less industry focus on its non-CO2 emissions, despite recent studies showing that these account for up to two-thirds of aviation’s climate impact...

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Aerospace - ISSN 2226-4310