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Aerospace, Volume 8, Issue 9

September 2021 - 42 articles

Cover Story: Hybrid rockets are an attractive technology for the future of commercial transportation in space due to their inherent safety and relatively low development cost. This paper reports on the change in velocity capability of a subcategory of hybrid rocket-based in-space transportation vehicles referred to as “post-boost stages” or “kick motors”. The impact of oxidizer selection, envelope shape, O/F-shift, and nozzle throat erosion on change in velocity are examined in detail. Hydrogen-peroxide-based motors are found to be most suitable when space is limited but propellant system mass is not, while nitrous oxide-based motors are found to be most suitable in the opposite case. View this paper
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Articles (42)

  • Article
  • Open Access
17 Citations
9,815 Views
20 Pages

Development of the EIRSAT-1 CubeSat through Functional Verification of the Engineering Qualification Model

  • Sarah Walsh,
  • David Murphy,
  • Maeve Doyle,
  • Jack Reilly,
  • Joseph Thompson,
  • Rachel Dunwoody,
  • Jessica Erkal,
  • Gabriel Finneran,
  • Gianluca Fontanesi and
  • Joseph Mangan
  • + 10 authors

8 September 2021

The Educational Irish Research Satellite (EIRSAT-1) is a 2U CubeSat developed at University College Dublin. The project aims to build, test, launch, and operate Ireland’s first satellite and to perform in-orbit demonstrations of three novel payloads...

  • Article
  • Open Access
29 Citations
5,978 Views
27 Pages

Hybrid Rockets as Post-Boost Stages and Kick Motors

  • Landon Kamps,
  • Shota Hirai and
  • Harunori Nagata

7 September 2021

Hybrid rockets are attractive as post-boost stages and kick motors due to their inherent safety and low cost, but it is not clear from previous research which oxidizer is most suitable for maximizing ΔV within a fixed envelope size, or what impact O/...

  • Article
  • Open Access
13 Citations
2,917 Views
22 Pages

6 September 2021

The problem of impact time control guidance with field-of-view constraint is addressed based on time-varying sliding mode control. The kinematic conditions that satisfy the impact time control with field-of-view constraint are defined, and then a nov...

  • Article
  • Open Access
10 Citations
6,510 Views
26 Pages

Effect of Reaction Wheel Imbalances on Attitude and Stabilization Accuracy

  • Stepan Tkachev,
  • Yaroslav Mashtakov,
  • Danil Ivanov,
  • Dmitry Roldugin and
  • Mikhail Ovchinnikov

6 September 2021

In this paper, the study of stabilization accuracy of a satellite equipped with a set of reaction wheels (RW) is presented. The model of motion takes into account possible static and dynamic reaction wheel imbalances. Due to the complexity of the mod...

  • Article
  • Open Access
16 Citations
6,638 Views
33 Pages

A Complete Mission Concept Design and Analysis of the Student-Led CubeSat Project: Light-1

  • Aaesha Almazrouei,
  • Aaliya Khan,
  • Abdulla Alhembar,
  • Ahmed Albuainain,
  • Ahmed Bushlaibi,
  • Ali Al Mahmood,
  • Ali Alqaraan,
  • Alya Alhammadi,
  • Amina AlBalooshi and
  • Ashraf Khater
  • + 19 authors

4 September 2021

Terrestrial gamma ray flashes (TGF) are intense and prompt bursts of X- and gamma-rays of up to 100 MeV of energy. Typically associated with thunderstorm activity, TGFs are produced by bremsstrahlung effects of electrons accelerated in strong electri...

  • Article
  • Open Access
9 Citations
2,840 Views
18 Pages

4 September 2021

This paper treats a robust adaptive trajectory-tracking control design for a rotorcraft using a high-fidelity math model subject to model uncertainties. In order to control the nonlinear rotorcraft model which shows strong inter-axis coupling and hig...

  • Article
  • Open Access
1 Citations
2,871 Views
17 Pages

4 September 2021

A comparison of d2 law and penetration length of biofuels with Jet–A through the incorporation of fuel properties and actual combustor inlet data at various flight trajectories is presented. This study aims to identify fuel properties and flight oper...

  • Article
  • Open Access
1 Citations
2,745 Views
27 Pages

4 September 2021

The present work focuses on the development of new mathematical and numerical tools to deal with wave propagation problems in a realistic liquid rocket chamber environment. A simplified real fluid equation of state is here derived, starting from the...

  • Article
  • Open Access
9 Citations
2,851 Views
20 Pages

3 September 2021

Performance of the traditional Kalman filter and its variants can seriously degrade when they are used to track a non-cooperative continuously thrusting spacecraft. To overcome this shortcoming, an adaptive tracking method for relative state estimati...

  • Article
  • Open Access
2 Citations
3,748 Views
27 Pages

3 September 2021

Assistant based speech recognition (ABSR) prototypes for air traffic controllers have demonstrated to reduce controller workload and aircraft flight times as a result. However, two aspects of ABSR could enhance benefits, i.e., (1) the predicted contr...

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Aerospace - ISSN 2226-4310