VSB-30 sounding rocket: History of flight performance

33Citations
Citations of this article
28Readers
Mendeley users who have this article in their library.
Get full text

Abstract

The VSB-30 vehicle is a two-stage, unguided, rail launched sounding rocket, consisting of two solid propellant motors, payload, with recovery and service system. By the end of 2010, ten vehicles had already been launched, three from Brazil (Alcântara) and seven from Sweden (Esrange). The objective of this paper is to give an overview of the main characteristics of the first ten flights of the VSB-30, with emphasis on performance and trajectory data. The circular 3σ dispersion area for payload impact point has around 50 km of radius. In most launchings of such vehicle, the impact of the payload fell within 2 sigma. This provides the possibility for further studies to decrease the area of dispersion from the impact point.

Cite

CITATION STYLE

APA

Garcia, A., Yamanaka, S. S. C., Barbosa, A. N., Bizarria, F. C. P., Jung, W., & Scheuerpflug, F. (2011). VSB-30 sounding rocket: History of flight performance. Journal of Aerospace Technology and Management, 3(3), 325–330. https://doi.org/10.5028/jatm.2011.03032211

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free