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Michael J. Brooks

Researcher at University of KwaZulu-Natal

Publications -  37
Citations -  838

Michael J. Brooks is an academic researcher from University of KwaZulu-Natal. The author has contributed to research in topics: Rocket & Sounding rocket. The author has an hindex of 8, co-authored 37 publications receiving 299 citations. Previous affiliations of Michael J. Brooks include University of Cape Town.

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Metal additive manufacturing in aerospace: A review

TL;DR: A comprehensive review of metal additive manufacturing in the aerospace industry can be found in this paper, where the primary application scenarios and the associated commercial and technical benefits of additive manufacturing for these applications are summarized.
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SAURAN : a new resource for solar radiometric data in Southern Africa

TL;DR: The Southern African Universities Radiometric Network (SAURAN) as discussed by the authors is an initiative of Stellenbosch University and the University of KwaZulu-Natal (UKZN), and consists of an initial set of ten ground stations equipped with secondary standard thermopile radiometers.
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An assessment of the solar resource for Durban, South Africa

TL;DR: In this article, a year-long data record of the solar flux intensity for the city of Durban (29°58′N 30°55′E) is presented, which is an example of a rapidly expanding urban center which can benefit from the implementation of solar energy technologies.
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A review of the performance and structural considerations of paraffin wax hybrid rocket fuels with additives

TL;DR: A review of existing regression rate measurement techniques on paraffin wax based fuels and the results obtained with various additives are collated and discussed in this paper as mentioned in this paper, including 2D slab motors that enable visualisation of liquefying fuel droplet entrainment and the effect of an increased viscosity on the droplet encoder mechanism, which can occur with the addition of structural enhancing polymers.
Proceedings ArticleDOI

Performance Modeling of a Paraffin Wax / Nitrous Oxide Hybrid Rocket Motor

TL;DR: In this article, a one-dimensional, non-steady flow predictive performance model for hybrid rocket motors is presented, which relies on basic thermodynamic and gas dynamic assumptions, and uses the NASA-CEA equilibrium chemistry code to determine gas combustion properties.