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Design improvement of air deployable parachute for high altitude launch ofpayload based on investigationand experimentation

Mahendra Pratap (DRDO, Aerial Delivery Research and Development Establishment , Agra, India)
Anil Kumar Agrawal (Department of Mechanical Engineering, IIT BHU , Varanasi, India)
Subhash Chandra Sati ( Research & Development Establishment (Engineers) Pune , DRDO, India)
Arun Kumar Saxena (DRDO, Aerial Delivery Research and Development Establishment , Agra, India)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 16 August 2021

Issue publication date: 30 November 2021

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Abstract

Purpose

The purpose of this paper is to improve the design of a solid square canopy of a parachute. The design improvements are brought out by providing minor slits in the canopy area. Proper designing of the parachute was carried out using theoretical investigation coupled with experimentation. This parachute is designed for launch of sonobuoy from fixed wing aircraft.

Design/methodology/approach

Literature review was carried out on the design of such parachutes for the launch of a sonobuoy from a high altitude to the water entry. Computational fluid dynamics (CFD) analysis provided the value of the coefficient of drag for the slit-cut square canopy parachute, with and without sonobuoy for different lengths of the slit. Besides the theoretical investigation, experimentation was also carried out to validate the design.

Findings

The experimentation was carried out on 58 and 75 gsm fabric canopies with the slit edge plain-cut with thermally sealed edges, stitched and strengthened. In the case of plain-cut slits on the canopy made of 75 gsm fabric, no tearing of the slit edge was observed in dynamic and flight tests.

Research limitations/implications

The present work has been carried out considering various assumptions and limited trial data specific to precision drop of 9 kg payload. The work can be adopted for bigger parachute for dropping of higher payloads.

Originality/value

Lab strength test, track dynamic and flight trials were conducted to acquire useful data for the present analysis. Besides the theoretical investigations and CFD analysis inherently based on numerous assumptions, experimentation was carried out as the sonobuoy deployment conditions are full of uncertainty. Dynamic and airdrop tests were conducted for this reason to determine design changes in the slits, both at the material level and on improvisations.

Keywords

Acknowledgements

The authors would like to thank Mr V.S. Verma, Scientist “G”, and his team for tireless scrutiny of this paper and suggestions. The authors extend their gratitude to staff and officers of TBRL, Chandigarh, India, for their efforts to conduct these trials. The authors sincerely offer their heartfelt thanks to the anonymous reviewers for their valuable comments to bring this research paper to its present level.

Conflict of interest None.

Citation

Pratap, M., Agrawal, A.K., Sati, S.C. and Saxena, A.K. (2021), "Design improvement of air deployable parachute for high altitude launch ofpayload based on investigationand experimentation", Aircraft Engineering and Aerospace Technology, Vol. 93 No. 10, pp. 1643-1655. https://doi.org/10.1108/AEAT-01-2021-0020

Publisher

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Emerald Publishing Limited

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