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Some typical solid propellant rocket motors

Report (2013)
Programme
Spacecraft Systems Engineering
Copyright: © 2013 Zandbergen, B.T.C.
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Published Date

31-12-2013

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Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Source:

Delft University of Technology, Faculty of Aerospace Engineering, Memorandum M-712 (Version 2.0)

Programme

Spacecraft Systems Engineering

Abstract

Typical Solid Propellant Rocket Motors (shortly referred to as Solid Rocket Motors; SRM's) are described with the purpose to form a database, which allows for comparative analysis and applications in practical SRM engineering.

Files

SOLID_M-712_December_2013.pdf
(pdf | 2.04 Mb)
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