PocketQube Deployment System

Master Thesis (2022)
Author(s)

A. Narayanan (TU Delft - Aerospace Engineering)

Contributor(s)

Sevket Uludag – Mentor (TU Delft - Space Systems Egineering)

J Guo – Mentor (TU Delft - Space Systems Egineering)

Faculty
Aerospace Engineering
Copyright
© 2022 Ashvij Narayanan
More Info
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Publication Year
2022
Language
English
Copyright
© 2022 Ashvij Narayanan
Graduation Date
08-06-2022
Awarding Institution
Delft University of Technology
Programme
Aerospace Engineering
Faculty
Aerospace Engineering
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Abstract

To enable greater access to space, this study aims to develop a cost-effective PocketQube Deployment System capable of deploying multiple PocketQubes from various launch vehicles. Mission cost, of which launch cost is a significant driver, can be reduced by minimizing deployment system mass. This can be achieved by structural analyses of single and multi pod configurations using finite element method. A metric called ‘deployer ratio’, defined as the ratio of payload and deployer mass, is introduced to compare the effectiveness of CubeSat and PocketQube deployers. From the perspective of deployer mass and mission cost, it was observed that it is more efficient to launch PocketQubes from a multi pod deployer rather than a single pod deployer. Although the estimated launch cost for PocketQubes is currently equivalent to commercial manufacturers, further cost reduction is possible by optimizing the mass of such a multi pod deployer.

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