Location of Repository

Rocket Engine Design

By Jakub Cejpek

Abstract

The objective of this study is to design a solid rocket fuel engine with sufficient power to propel 500 grams to 1500 meters of altitude. Furthermore to draft a design of a rocket that will utilize this category of solid rocket fuel engine. This study will begin with a theoretical exploration of the means to formulate the correct propellant closest to the theoretical solid rocket fuel formula. This section of the exploration will exclude the construction materials, technology, and the propellant availability. After the theoretical exploration the calculations will continue, respecting the availability of construction materials, technology, and the propellant; to investigate the means to formulate the correct propellant closest to the theoretical formula. Then, according to the new propellant formulation, re-design the engine

Topics: vibration exciter; rocket; tuhá pohonná hmota; rocket engine; raketa; solid propellant; impulsní raketový budič; raketový motor
Publisher: Vysoké učení technické v Brně. Fakulta strojního inženýrství
Year: 2009
OAI identifier: oai:invenio.nusl.cz:211449
Download PDF:
Sorry, we are unable to provide the full text but you may find it at the following location(s):
  • http://www.nusl.cz/ntk/nusl-21... (external link)
  • Suggested articles


    To submit an update or takedown request for this paper, please submit an Update/Correction/Removal Request.