Development of a rocket recovery system

The design, fabricate and testing of a rocket recovery system is presented in this report. Recovery system is important for a rocket for low cost of fabricating the rocket and the flight data analysis. The recovery system chosen for the rocket is a parachute recovery system. The recovery system is d...

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Bibliographic Details
Main Author:	Nur Fitrina, Mat Nawi
Format:	Undergraduates Project Papers
Language:	English
Published:	2013
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://umpir.ump.edu.my/id/eprint/8659/ http://umpir.ump.edu.my/id/eprint/8659/ http://umpir.ump.edu.my/id/eprint/8659/1/cd8162.pdf

id	ump-8659
recordtype	eprints
spelling	ump-86592015-11-02T01:47:53Z http://umpir.ump.edu.my/id/eprint/8659/ Development of a rocket recovery system Nur Fitrina, Mat Nawi TL Motor vehicles. Aeronautics. Astronautics The design, fabricate and testing of a rocket recovery system is presented in this report. Recovery system is important for a rocket for low cost of fabricating the rocket and the flight data analysis. The recovery system chosen for the rocket is a parachute recovery system. The recovery system is divided into two parts; the parachute and the ejection system. In this report, six different designs are fabricated. Drop test of the parachutes was conducted to find the design for the parachute. The test shows that the semi- ellipsoidal parachute is the best parachute that can support an empty rocket mass of 2.5kg with the descent range is 5.98m/s. The parachute recovery system constructed in this project will be integrated with the rocket body and powered by a solid propellent rocket motor. 2013-01 Undergraduates Project Papers NonPeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/8659/1/cd8162.pdf Nur Fitrina, Mat Nawi (2013) Development of a rocket recovery system. Faculty of Mechanical Engineering, Universiti Malaysia Pahang. http://iportal.ump.edu.my/lib/item?id=chamo:82992&theme=UMP2
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Malaysia Pahang
building	UMP Institutional Repository
collection	Online Access
language	English
topic	TL Motor vehicles. Aeronautics. Astronautics
spellingShingle	TL Motor vehicles. Aeronautics. Astronautics Nur Fitrina, Mat Nawi Development of a rocket recovery system
description	The design, fabricate and testing of a rocket recovery system is presented in this report. Recovery system is important for a rocket for low cost of fabricating the rocket and the flight data analysis. The recovery system chosen for the rocket is a parachute recovery system. The recovery system is divided into two parts; the parachute and the ejection system. In this report, six different designs are fabricated. Drop test of the parachutes was conducted to find the design for the parachute. The test shows that the semi- ellipsoidal parachute is the best parachute that can support an empty rocket mass of 2.5kg with the descent range is 5.98m/s. The parachute recovery system constructed in this project will be integrated with the rocket body and powered by a solid propellent rocket motor.
format	Undergraduates Project Papers
author	Nur Fitrina, Mat Nawi
author_facet	Nur Fitrina, Mat Nawi
author_sort	Nur Fitrina, Mat Nawi
title	Development of a rocket recovery system
title_short	Development of a rocket recovery system
title_full	Development of a rocket recovery system
title_fullStr	Development of a rocket recovery system
title_full_unstemmed	Development of a rocket recovery system
title_sort	development of a rocket recovery system
publishDate	2013
url	http://umpir.ump.edu.my/id/eprint/8659/ http://umpir.ump.edu.my/id/eprint/8659/ http://umpir.ump.edu.my/id/eprint/8659/1/cd8162.pdf
first_indexed	2023-09-18T22:06:28Z
last_indexed	2023-09-18T22:06:28Z
_version_	1777414741684125696

Development of a rocket recovery system

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