期刊名称：International Journal of Innovative Research in Science, Engineering and Technology
印刷版ISSN：2347-6710
电子版ISSN：2319-8753
出版年度：2016
卷号：5
期号：6
页码：10829
DOI：10.15680/IJIRSET.2015.0506233
出版社：S&S Publications
摘要：The payload performance analysis of the typical sounding rocket has been taken for observation in thispaper. Payload of any rocket depicts the objective of the mission. This payload is more effective in determining thepeak parameters of the rocket such as the peak altitude and the impact range. The peak parameters of the typicalsounding rockets have been found for varied payloads with varied launch elevation angles (LEA). The Payloads takenfor analysis are 50,100,150,200 and 250 kg. The LEAs taken for the analysis are 77,78,79,80 and 81 degrees. It isobserved that the peak parameters have a heavy impact over the payloads and LEA variations leading to a drasticchange. The analysis was done using 6-DoF performance simulator.
关键词：sounding rocket; launch elevation angle; payloads; six degrees of freedom; peak altitude and impact;range.
