Modern Propulsions for Aerospace-Part II

Journal of Aircraft and Spacecraft Technology, 2017, 1(1)

9 Pages Posted: 22 Nov 2017

See all articles by Relly Victoria Petrescu

Relly Victoria Petrescu

Polytechnic University of Bucharest - ARoTMM-IFToMM

Raffaella Aversa

Advanced Material Lab - Department of Architecture and Industrial Design

B. Akash

American University of Ras Al Khaimah

Ronald Bucinell

Union College

Juan Corchado

University of Salamanca

Filippo Berto

Norwegian University of Science and Technology (NTNU) - Department of Engineering Design and Materials

MirMilad Mirsayar

Texas A&M University - Department of Civil Engineering

Antonio Apicella

Advanced Material Lab - Department of Architecture and Industrial Design

Florian Ion Petrescu

Polytechnic University of Bucharest - ARoTMM-IFToMM

Date Written: November 19, 2017

Abstract

Speaking about a new engine ionic means to speak about a new aircraft. The paper presents in a short time the actual engines ion chambers (called the ion thrusters) and other new ionic motors proposed by the authors. The engine (ionic propulsion unit of ions, that accelerates the positive ions through a potential difference) is approximately ten times more efficient than classic system based on combustion. We can further improve the efficiency of the 10-50 times in the case in which is used the pulses of positive ions accelerated in a cyclotron mounted on the ship; efficiency may increase with ease of a thousand times in the case in which the positive ions will be accelerate in a synchrotron high energy, synchrocyclotron or isochronous cyclotron (1-100 GeV). For this, the great classic synchrotron is reduced to a surface-ring (magnetic core). The future (ionic) engine will have a circular particle binding (energy high or very high speed). Thus we can increase the speed and autonomy of the vessel, using a smaller quantity of fuel. It can be used a radiation synchrotron (synchrotron high intensity), with X-ray or gamma radiation. In this case, will result in a beam engine with the wiring (not an ionic engine), which will use only the power (energy, which may be solar energy, nuclear energy, or a combination) and so we will eliminate the fuel. It is suggested to use a powerful LINAC at the outlet of the synchrotron (especially when one accelerates the electron beam) in order not to lose power by photons of the emission premature. With a new ionic engine practically builds a brand new aircraft that can move through the water and air with the same ease. This new aircraft will be able to expedite directly, without an engine with the additional combustion and without the gravity assistance.

Note: © 2017 Relly Victoria Virgil Petrescu, Raffaella Aversa, Bilal Akash, Ronald Bucinell, Juan Corchado, Filippo Berto, MirMilad Mirsayar, Antonio Apicella and Florian Ion Tiberiu Petrescu. This is an open access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.

Suggested Citation

Petrescu, Relly Victoria and Aversa, Raffaella and Akash, B. and Bucinell, Ronald and Corchado, Juan and Berto, Filippo and Mirsayar, MirMilad and Apicella, Antonio and Petrescu, Florian Ion, Modern Propulsions for Aerospace-Part II (November 19, 2017). Journal of Aircraft and Spacecraft Technology, 2017, 1(1). Available at SSRN: https://ssrn.com/abstract=3073973

Relly Victoria Petrescu

Polytechnic University of Bucharest - ARoTMM-IFToMM ( email )

Romania

Raffaella Aversa

Advanced Material Lab - Department of Architecture and Industrial Design ( email )

81031 Aversa (CE)
Italy

B. Akash

American University of Ras Al Khaimah ( email )

American University of Ras Al Khaimah
School of Graduate Studies and Research
Ras Al Khaimah, RAK 10021
United Arab Emirates

HOME PAGE: http://www.aurak.ac.ae

Ronald Bucinell

Union College ( email )

Schenectady, NY 12308-3151
United States

Juan Corchado

University of Salamanca ( email )

Campus Miguel de Unamuno
ES-37007 Salamanca, Salamanca 23007
Spain

Filippo Berto

Norwegian University of Science and Technology (NTNU) - Department of Engineering Design and Materials ( email )

Trondheim
Norway

MirMilad Mirsayar

Texas A&M University - Department of Civil Engineering ( email )

College Station, TX
United States

Antonio Apicella

Advanced Material Lab - Department of Architecture and Industrial Design ( email )

81031 Aversa (CE)
Italy

Florian Ion Petrescu (Contact Author)

Polytechnic University of Bucharest - ARoTMM-IFToMM ( email )

Romania

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