Chemical Rocket Motors for Space Launch Applications: Parametric Approach-Reference-Cited by-同舟云学术

Chemical Rocket Motors for Space Launch Applications: Parametric Approach

Published:2022-04-01 Issue:1 Volume:8 Page:48-51
ISSN:
Container-title:1
language:
Short-container-title:JEMM

Author:

Janani Kavipriya VS¹,Akshay Masetty¹,Mane Shreya¹,Dipak Jadhav Shruti¹

Affiliation:

1. Department of Research and Development, ASTROEX RESEARCH ASSOCIATION, Deoria, India

Abstract

Hybridrocket motors are widely used in heavy launch vehicles with maximum payload capacity. The main reason for the study in this field is that the hybrid rocket motor is very easy to handle and has a simple design. In this paper, we have studied the parameters involved in designing and optimizing the hybrid rockets which provides in achieving maximum performance value. The several parameters considered for parameters involve are- burn rate, specific fuel consumption, specific impulse, efficiency. The design constraints will be responsible in achieving a high thrust level through the nozzle. The study also highlights the propellants being used in hybrid rocket motor. The collaborative research will aid in briefing the design and the working of the hybrid motors that is frequently being utilized in the industry.

Publisher

REST Publisher

Reference27 articles.

1. Ankit Kumar Mishra, Rishi Suhas Karandikar, Janani Kavipriya V.S, “Study of nozzle flow separations in divergent section of nozzle”, International Journal of Universal Science and Engineering, vol. no. 7, Jan-Dec, 2021

2. Ankit Kumar Mishra, Janani Kavipriya.V.S, “A Technical review on effect of spray angles and characteristics for a pintle injector”, Journal of Advanced Engineering Research, vol.7, no.2, pp. 30-36, 2020.

3. Ankit Kumar Mishra, Madhumitha M, Vaishnavi Shenoy “Numerical and Computational Analysis on Two Stage Sounding Rocket”, International Journal of Science, Engineering and Technology, vol. 9(4), pp. 01-06, 2021.

4. Ankit Kumar Mishra, Kshitij Gandhi, Kuldeep Sharma, Neerumalla Sumanth, “Conceptual design and analysis of two stage sounding rocket”, International Journal of Universal Science and Engineering, vol.7(1), pp. 52-72, 2021.

5. Ankit Kumar Mishra, Amandeep Singh, “Computational fluid dynamics analysis on the convergent nozzle design”, International Journal of Advances in Engineering Research, vol. 20(3), pp. 01-06, 2020.