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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 02 | Feb -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1881
Demonstration of Electromagnetic Phenomenon for Point Object
Launching
Aditya Bagwe1, Dinesh Nair2, A. N. Pimpale3, Shashi Prabha4
1 B.E. Student, Dept. of EE, MGM college of Engineering & Technology Maharashtra, India
2 B.E. Student, Dept. of EE, MGM college of Engineering & Technology Maharashtra,India
3 Lecturer, Dept. of ExTc , Yadavrao Tasgaonkar Polytechnic, Karjat, Maharashtra, India
4 Professor, Dept. of EE , MGM college of Engineering & Technology Maharashtra,India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - Electromagnetic engineering plays an
important role in study of three dimensional real time
applications. Electromagnetic phenomenon has wide range
of applications like power grids, submarines, broadcasting,
RADAR & satellites. This paper reviews application area in
electromagnetic rail gun & also demonstrates
electromagnetism in launch of object of rail gun projectile.
Design details of control mechanism to interface
electromagnetic system with microcontroller & wireless
module discussed.
Key Words: EMRG, Projectile launching, Rail gun
design
1. INTRODUCTION
At the early start of 19th century development of
electromagnetic rail gun started. But it gained
popularity during World War II as a weapon to target
enemies. Now a day’s rail gun considered as future
space vehicle. Construction of large models of EMRG
(Electromagnetic Rail Gun) is complicated & tedious
job. Hence plenty of demonstrations has implanted in
small sizes of EMRG. Its point form energy
considerations are taken in account as design
parameters.Maindesignaspectsarepairofparallelrail
tracks, projectile, coil gun capacitor banks, charging
circuits, & DC power source. [1]
Such electromagnetic assembly usually controlled by
electrical power assemblies [2]. Here interfacing of
EMRG with microcontroller represented & operated it
with RF trans- receiver module.
Power required for controlling of EMRG is small, as it
operates only on +5 V dc supply. Transmitted DC
pulses encoded using HT12D encoder circuit. Pulses
received at receiver end decoded using decoder pair &
transferred to MCU unit. According to command set
from transmitter MCU unit provides pulses to EMRG
unit. Relay acts as isolators in between EMRG unit &
MCU. Wireless RFmoduleunithasisolationinbetween
controlling transmitter & operational receiver.
1.1 Principle of operation:-
Fig. 1 Basic principle of EMRG
Due to the Faradays law of electromagnetic induction,
magnetism produced in electric bars or rail. This
magnetism results in a force.
[1]
The application can be understood with the help of
Biot-Savart law &, Laplace or Lorentz force equation.
[2]
[3]
[4]
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 02 | Feb -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1882
Here F is the force on projectile; B is magnetic field
density with u as permittivity of magnetic material.
1.2 Launch of projectile:-
Fig. 2 Launch of projectile with EMRG
In many of the large scale experiments projectile tried
to launch in space in vertical direction. As our
projectile size is considerably small, we tried to launch
the projectile in linear or horizontal direction.
Launching task is the operation of driving current
through electric bars. It is essential to useheavypower
supply. Some laboratory experiments achieved high
speed launching due to large energy supplying power
supplies. Ian R. McNab archived muzzle velocity of 2-3
km/s for more than 8MJ energies. Theoretically it can
be extended up to 7.5 Km/s for 10GJ of energy for
space vehicle launching. Due to increase in theoretical
muzzle velocity and range, rail gun has advantageous
over chemical propellant based methods. [3]
2. Design Considerations:-
It is found that for the production of uniform magnetic
field, solid wires should be preferred. Air filled within
the rails makes magnetic field non-uniform. Projectile
accelerates more in certain direction due to
concentrated uniform magnetic field. [4]
Rail gun has structure of two conducting rails fitted
with armature which completed the circuit. Current
carrying capacityoftherailbarschosenshouldbehigh.
It is because current in bars results in force acting on
projectile in the field. In order to develop dense
magnetic field in armature high permeabilitymagnetic
material should be selected. Rail should not make
contact with armature but keep thematshortdistance.
Armature should be solid. [3, 6]
In order to design power supply for EMRG, it should
provide high current. For actuationofcoils,thecurrent
pulses are generated on which actuator relays
operated. It is not possible to design power supply
which will providehighcurrent.Hencecapacitorbanks
are designed. Capacitors store large amount of energy
in the form of electric field & discharges in form of
current which is high in accordance with value of
capacitors used.
Projectile must fit tightly into the barrel. Material
selection for projectile & barrel depends on the
strength & life of the EMRG. Assembly should be
assembled tightly to reduce mechanical & highcurrent
magnetizing & hysteresis losses. [6]
2.1 Proposed Demonstration design:-
Proposed demonstration system based on the
prototype design of electromagneticrailgunforlaunch
of point mass projectile. For producing strong
electromagnetism instead of capacitor banks, 18 V
battery power supply selected. For avoiding sudden
discharge of battery, three series connected 6V / 4.5
AH lead acid rechargeable batteries connected in
series.
Fig. 3 Circuit diagram of Tx unit in EMRG
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 02 | Feb -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1883
Fig. 4 Circuit diagram of Rx unit in EMRG
Control mechanism of the rail gun operated from
AT89S52 microcontroller. Benefit of using such basic
microcontroller is its available software & firmware
support. It is programmed by usingKeiluvision4IDE&
Proload downloader.
Four copper coils of having 250 number turns on each
coil wounded PVC bore material. For better operation
we use a 16 SWG wire for making the coils. It has
currentcarrying capacityof 18 A & only 1 Ω resistance.
Projectile used for launching is of capsule size&ofiron
material. It is of 50 gram small weight, 0.5 projectile
diameters. Efficient distance travelled by this
consideration with muzzle velocity is 60 feet. Launch
of projectile done through 50 cm length PVC tube.
Fig.5 Designed coli unit for demonstration
Electromagnetic types of relays are used as contactors
& driving mechanism. These relays also provide
isolation between electromagneticfunctioningrailgun
unit & control unit.
As effective distance covered by this demonstration is
small, a wireless module operating on 433 MHz used
for operation. This is interfaced with MCU unit with
HT12D decoder unit at receiver side. Same Encoder &
Transmitter module interfaced with switches to
perform firing & timing up-down operation.
Design cost of such system is larger but it is effective
option for operation with RF module interface. Such
system can be used in automation without human
presence.
3. CONCLUSIONS
Electromagnetism has large influence on rail gun
mechanism. Designed prototype model works well for
point launch of object up to 60 feet distance only.
Increase of distance & muzzle velocity is possible with
considerable changes in conductivity of coil material.
Low Powered EMRG can be controlled & operated by
using MCU unit & wireless devices. In future
electromagnetic systems can be efficiently interfaced
with WSN networks & launching from any space
module is possible.
ACKNOWLEDGEMENT
This research was supported by Staff members of
Electrical department of “MGM college of Engineering,
Mumbai.” We specially thanks our faculty “Dr. Uma
Mukharji ” for generating interest in research area of
electromagnetic.
REFERENCES
[1] M. R. Palmer and A. E. Dabiri, “Electromagnetic
space launch: A re-evaluation in light of current
technology and launch needs and feasibility of a near-
term demonstration,” IEEE Trans. Magn., vol. 25, pp.
393–399, Jan. 1989.
[2] B. Turman, “Long range naval coilgun technology,”
Presentation to NSWL, Dahlgren, VA, Feb. 21, 2001.
[3] I. R. McNab and G. A. Kemeny, “Electromagnetic
projectile launcher with combination plasma
/conductor armature,” U.S. Patent 4 467 696, Aug. 28,
1984.
[4] W. A. Jacobs, "MagneticlaunchAssist-NASA'sVision
for the Future” IEEE Trans. Magn., Vol. 37, pp. 55-57,
Jan. 2001.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 02 | Feb -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1884
[5] Salami, S.O, Green O.O, Philips D.A “Design and
Simulation of a Rail Gun using Microcontroller” IJRITT
Volume: 01 Issue: 07 November – 2015
6] Scott Harmon “A Look into Railgun Physics and
Design” Senior Honors Thesis April 2011
7] Uma Mukherji “Electromagnetic field theory&wave
propagation” Narosa Publication, 2006
BIOGRAPHIES
Aditya Bagawe is currently
pursuing B.E. ( Electrical ) in MGM
College of Engineering Mumbai. He
has completed his diploma in
Electrical engineering with first
class.
Dinesh Nair is currently pursuing
B.E. ( Electrical ) in MGM College of
Engineering Mumbai.
Mr. A. N. Pimpale received M. Tech
degree in digital communication
from RGPV Bhopal (India).
Currently he is working as a
lecturer in YTP (ExTc) Karjat,
Maharashtra (India).
Mrs. Shashi Prapha has 26 years of
teaching experience in Control
System. She has completed her M.
Tech in control Systems from VJTI
Mumbai ( India).

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Demonstration of Electromagnetic Phenomenon for Point Object Launching

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 02 | Feb -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1881 Demonstration of Electromagnetic Phenomenon for Point Object Launching Aditya Bagwe1, Dinesh Nair2, A. N. Pimpale3, Shashi Prabha4 1 B.E. Student, Dept. of EE, MGM college of Engineering & Technology Maharashtra, India 2 B.E. Student, Dept. of EE, MGM college of Engineering & Technology Maharashtra,India 3 Lecturer, Dept. of ExTc , Yadavrao Tasgaonkar Polytechnic, Karjat, Maharashtra, India 4 Professor, Dept. of EE , MGM college of Engineering & Technology Maharashtra,India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - Electromagnetic engineering plays an important role in study of three dimensional real time applications. Electromagnetic phenomenon has wide range of applications like power grids, submarines, broadcasting, RADAR & satellites. This paper reviews application area in electromagnetic rail gun & also demonstrates electromagnetism in launch of object of rail gun projectile. Design details of control mechanism to interface electromagnetic system with microcontroller & wireless module discussed. Key Words: EMRG, Projectile launching, Rail gun design 1. INTRODUCTION At the early start of 19th century development of electromagnetic rail gun started. But it gained popularity during World War II as a weapon to target enemies. Now a day’s rail gun considered as future space vehicle. Construction of large models of EMRG (Electromagnetic Rail Gun) is complicated & tedious job. Hence plenty of demonstrations has implanted in small sizes of EMRG. Its point form energy considerations are taken in account as design parameters.Maindesignaspectsarepairofparallelrail tracks, projectile, coil gun capacitor banks, charging circuits, & DC power source. [1] Such electromagnetic assembly usually controlled by electrical power assemblies [2]. Here interfacing of EMRG with microcontroller represented & operated it with RF trans- receiver module. Power required for controlling of EMRG is small, as it operates only on +5 V dc supply. Transmitted DC pulses encoded using HT12D encoder circuit. Pulses received at receiver end decoded using decoder pair & transferred to MCU unit. According to command set from transmitter MCU unit provides pulses to EMRG unit. Relay acts as isolators in between EMRG unit & MCU. Wireless RFmoduleunithasisolationinbetween controlling transmitter & operational receiver. 1.1 Principle of operation:- Fig. 1 Basic principle of EMRG Due to the Faradays law of electromagnetic induction, magnetism produced in electric bars or rail. This magnetism results in a force. [1] The application can be understood with the help of Biot-Savart law &, Laplace or Lorentz force equation. [2] [3] [4]
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 02 | Feb -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1882 Here F is the force on projectile; B is magnetic field density with u as permittivity of magnetic material. 1.2 Launch of projectile:- Fig. 2 Launch of projectile with EMRG In many of the large scale experiments projectile tried to launch in space in vertical direction. As our projectile size is considerably small, we tried to launch the projectile in linear or horizontal direction. Launching task is the operation of driving current through electric bars. It is essential to useheavypower supply. Some laboratory experiments achieved high speed launching due to large energy supplying power supplies. Ian R. McNab archived muzzle velocity of 2-3 km/s for more than 8MJ energies. Theoretically it can be extended up to 7.5 Km/s for 10GJ of energy for space vehicle launching. Due to increase in theoretical muzzle velocity and range, rail gun has advantageous over chemical propellant based methods. [3] 2. Design Considerations:- It is found that for the production of uniform magnetic field, solid wires should be preferred. Air filled within the rails makes magnetic field non-uniform. Projectile accelerates more in certain direction due to concentrated uniform magnetic field. [4] Rail gun has structure of two conducting rails fitted with armature which completed the circuit. Current carrying capacityoftherailbarschosenshouldbehigh. It is because current in bars results in force acting on projectile in the field. In order to develop dense magnetic field in armature high permeabilitymagnetic material should be selected. Rail should not make contact with armature but keep thematshortdistance. Armature should be solid. [3, 6] In order to design power supply for EMRG, it should provide high current. For actuationofcoils,thecurrent pulses are generated on which actuator relays operated. It is not possible to design power supply which will providehighcurrent.Hencecapacitorbanks are designed. Capacitors store large amount of energy in the form of electric field & discharges in form of current which is high in accordance with value of capacitors used. Projectile must fit tightly into the barrel. Material selection for projectile & barrel depends on the strength & life of the EMRG. Assembly should be assembled tightly to reduce mechanical & highcurrent magnetizing & hysteresis losses. [6] 2.1 Proposed Demonstration design:- Proposed demonstration system based on the prototype design of electromagneticrailgunforlaunch of point mass projectile. For producing strong electromagnetism instead of capacitor banks, 18 V battery power supply selected. For avoiding sudden discharge of battery, three series connected 6V / 4.5 AH lead acid rechargeable batteries connected in series. Fig. 3 Circuit diagram of Tx unit in EMRG
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 02 | Feb -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1883 Fig. 4 Circuit diagram of Rx unit in EMRG Control mechanism of the rail gun operated from AT89S52 microcontroller. Benefit of using such basic microcontroller is its available software & firmware support. It is programmed by usingKeiluvision4IDE& Proload downloader. Four copper coils of having 250 number turns on each coil wounded PVC bore material. For better operation we use a 16 SWG wire for making the coils. It has currentcarrying capacityof 18 A & only 1 Ω resistance. Projectile used for launching is of capsule size&ofiron material. It is of 50 gram small weight, 0.5 projectile diameters. Efficient distance travelled by this consideration with muzzle velocity is 60 feet. Launch of projectile done through 50 cm length PVC tube. Fig.5 Designed coli unit for demonstration Electromagnetic types of relays are used as contactors & driving mechanism. These relays also provide isolation between electromagneticfunctioningrailgun unit & control unit. As effective distance covered by this demonstration is small, a wireless module operating on 433 MHz used for operation. This is interfaced with MCU unit with HT12D decoder unit at receiver side. Same Encoder & Transmitter module interfaced with switches to perform firing & timing up-down operation. Design cost of such system is larger but it is effective option for operation with RF module interface. Such system can be used in automation without human presence. 3. CONCLUSIONS Electromagnetism has large influence on rail gun mechanism. Designed prototype model works well for point launch of object up to 60 feet distance only. Increase of distance & muzzle velocity is possible with considerable changes in conductivity of coil material. Low Powered EMRG can be controlled & operated by using MCU unit & wireless devices. In future electromagnetic systems can be efficiently interfaced with WSN networks & launching from any space module is possible. ACKNOWLEDGEMENT This research was supported by Staff members of Electrical department of “MGM college of Engineering, Mumbai.” We specially thanks our faculty “Dr. Uma Mukharji ” for generating interest in research area of electromagnetic. REFERENCES [1] M. R. Palmer and A. E. Dabiri, “Electromagnetic space launch: A re-evaluation in light of current technology and launch needs and feasibility of a near- term demonstration,” IEEE Trans. Magn., vol. 25, pp. 393–399, Jan. 1989. [2] B. Turman, “Long range naval coilgun technology,” Presentation to NSWL, Dahlgren, VA, Feb. 21, 2001. [3] I. R. McNab and G. A. Kemeny, “Electromagnetic projectile launcher with combination plasma /conductor armature,” U.S. Patent 4 467 696, Aug. 28, 1984. [4] W. A. Jacobs, "MagneticlaunchAssist-NASA'sVision for the Future” IEEE Trans. Magn., Vol. 37, pp. 55-57, Jan. 2001.
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 02 | Feb -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1884 [5] Salami, S.O, Green O.O, Philips D.A “Design and Simulation of a Rail Gun using Microcontroller” IJRITT Volume: 01 Issue: 07 November – 2015 6] Scott Harmon “A Look into Railgun Physics and Design” Senior Honors Thesis April 2011 7] Uma Mukherji “Electromagnetic field theory&wave propagation” Narosa Publication, 2006 BIOGRAPHIES Aditya Bagawe is currently pursuing B.E. ( Electrical ) in MGM College of Engineering Mumbai. He has completed his diploma in Electrical engineering with first class. Dinesh Nair is currently pursuing B.E. ( Electrical ) in MGM College of Engineering Mumbai. Mr. A. N. Pimpale received M. Tech degree in digital communication from RGPV Bhopal (India). Currently he is working as a lecturer in YTP (ExTc) Karjat, Maharashtra (India). Mrs. Shashi Prapha has 26 years of teaching experience in Control System. She has completed her M. Tech in control Systems from VJTI Mumbai ( India).