Gas Pressure Measurement On Rocket Chamber Based On Strain Gauge Sensor

Authors

  • Anggara Trisna Nugraha Politeknik Perkapalan Negeri Surabaya
  • Rahman Arifuddin Universitas Merdeka Malang

DOI:

https://doi.org/10.26905/jeemecs.v3i2.4585

Keywords:

Roket, MPXV7002DP, Chamber, Arduino Uno

Abstract

The use of rocket technology is currently also widely used for research. The rocket itself is a flying vehicle that moves by getting a boost through the combustion reaction that occurs in the rocket. The rocket itself can launch the load to the desired destination. In the field of science and technology, continuous efforts are required to realize the development of this rocket in order to achieve independence and prosperity. In the field of science and technology, continuous efforts are required to realize the development of this rocket in order to achieve independence and prosperity. The implementation of the strain gauge sensor through the MPXV7002DP gas pressure sensor obtained the amount of gas pressure during the combustion of the propellant in the rocket chamber, where the gas pressure can be measured, processed through the Arduino Uno microcontroller. The system can measure the maximum pressure up to 380 kPa and then the system can check any changes in voltage level to prove if there is a leak in the rocket.


Author Biography

Anggara Trisna Nugraha, Politeknik Perkapalan Negeri Surabaya

Bachelor's Degree Electrical Engineering at Jember University. Master's Degree Electrical Engineering Sub. Control Engineering at Sepuluh Nopember Institute of Technology. Lecturer in D4 Marine electrical Engineering at Shipbuilding Institute of Polytechnic Surabaya.

References

M. Oschwald et al., “Measurement of heat transfer in liquid rocket combustors,†High Pressure Flows for Propulsion Applications, vol. 260. Progress in Astronautics and Aeronautics, AIAA Reston, VA, pp. 281–332, 2020.

F. Hötte, T. Fiedler, M. C. Haupt, P. Lungu, C. V Sethe, and O. J. Haidn, “Experimental Investigations of Thermomechanical Fluid–Structure Interaction in Rocket Combustion Chambers,†J. Propuls. Power, vol. 35, no. 5, pp. 906–916, 2019.

H. Lin, F. Liu, Y. Dai, and A. Zhou, “Cascaded fiber Mach–Zehnder interferometers for Sensitivity-enhanced gas pressure measurement,†IEEE Sens. J., vol. 19, no. 7, pp. 2581–2586, 2018.

L. Zhang, S. Guo, H. Yu, and Y. Song, “Performance evaluation of a strain-gauge force sensor for a haptic robot-assisted catheter operating system,†Microsyst. Technol., vol. 23, no. 10, pp. 5041–5050, 2017.

A. T. Nugraha and T. Agustinah, “Quadcopter path following control design using output feedback with command generator tracker based on LOS,†in 2017 International Seminar on Intelligent Technology and Its Applications (ISITIA), 2017, pp. 255–260.

H. Li et al., “A Supersensitive, Multidimensional Flexible Strain Gauge Sensor Based on Ag/PDMS for Human Activities Monitoring,†Sci. Rep., vol. 10, no. 1, pp. 1–9, 2020.

K. Nelson and K. Mohseni, “An artificial fish lateral line sensory system composed of modular pressure sensor blocks,†in 2017 IEEE International Conference on Robotics and Automation (ICRA), 2017, pp. 4914–4919.

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Published

2020-08-30

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Section

Articles