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Design and development of a payload module for rocket-borne experiments for university students (REXUS)

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dc.contributor.author Ukwatta, UDAK
dc.contributor.author Khangamage, UP
dc.contributor.author Fernando, P
dc.date.accessioned 2013-10-21T02:13:00Z
dc.date.available 2013-10-21T02:13:00Z
dc.date.issued 2009
dc.identifier.uri http://dl.lib.mrt.ac.lk/handle/123/8295
dc.description.abstract Sounding rockets are the most common medium that are used carry instruments to near space for various types of experiments such as microgravity experiments, upper atmospheric experiments etc. However, due to high acceleration and vibration occurred, most of the instruments tend to give inaccurate or imprecise results. Hence, there is a real need in developing a proper payload carrying unit, which can protect instruments from undesirable effects, in sounding rockets. This paper presents an improved design for a payload carrying module developed.
dc.language en
dc.title Design and development of a payload module for rocket-borne experiments for university students (REXUS)
dc.type Conference-Extended-Abstract
dc.identifier.year 2009
dc.identifier.conference Research for Industry
dc.identifier.place Faculty of Engineering, University of Moratuwa
dc.identifier.pgnos pp. 103-105
dc.identifier.proceeding 15th Annual symposium on Research and Industry


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