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Parameterization and geometric optimization of balloon launched sensorcraft for atmospheric research missions

Parameterization and geometric optimization of balloon launched sensorcraft for atmospheric research missions
Parameterization and geometric optimization of balloon launched sensorcraft for atmospheric research missions
We present a method for the payload centric automated design and manufacturing of balloon launched, high altitude gliders. The purpose of these gliders is to conduct directed measurements of atmospheric phenomena with a variety of payloads. A bespoke airframe design is generated that can protect the payload, ensure recoverability and extend sampling times. A manufacturing technique, that relies heavily on rapid prototyping, allows for rapid realization of the aircraft design. This allows atmospheric scientists and researchers unprecedented access to a broad range of altitudes.
Paulson, Christopher
264d154a-07d6-4272-aefc-e645c78878bd
Sobester, Andras
096857b0-cad6-45ae-9ae6-e66b8cc5d81b
Paulson, Christopher
264d154a-07d6-4272-aefc-e645c78878bd
Sobester, Andras
096857b0-cad6-45ae-9ae6-e66b8cc5d81b

Paulson, Christopher and Sobester, Andras (2013) Parameterization and geometric optimization of balloon launched sensorcraft for atmospheric research missions. 51st AIAA Aerospace Sciences Meeting, Grapevine, United States. 07 - 10 Jan 2013. 11 pp .

Record type: Conference or Workshop Item (Paper)

Abstract

We present a method for the payload centric automated design and manufacturing of balloon launched, high altitude gliders. The purpose of these gliders is to conduct directed measurements of atmospheric phenomena with a variety of payloads. A bespoke airframe design is generated that can protect the payload, ensure recoverability and extend sampling times. A manufacturing technique, that relies heavily on rapid prototyping, allows for rapid realization of the aircraft design. This allows atmospheric scientists and researchers unprecedented access to a broad range of altitudes.

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More information

Published date: 10 January 2013
Venue - Dates: 51st AIAA Aerospace Sciences Meeting, Grapevine, United States, 2013-01-07 - 2013-01-10
Organisations: Computational Engineering & Design Group

Identifiers

Local EPrints ID: 349102
URI: http://eprints.soton.ac.uk/id/eprint/349102
PURE UUID: 19eb18a4-9636-4521-8644-a2758bac8050
ORCID for Andras Sobester: ORCID iD orcid.org/0000-0002-8997-4375

Catalogue record

Date deposited: 26 Feb 2013 14:16
Last modified: 15 Mar 2024 03:13

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Contributors

Author: Christopher Paulson
Author: Andras Sobester ORCID iD

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