WUSAT-1 CubeSat Mission

WUSAT-1 1U Platform

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WUSAT-1 CubeSat

Years of Operation: 2012 - 2013

Client: None - Prototype Trial

Mission: - First prototype single unit (1U) CubeSat via high-altitude balloon launch

Partners: RS ComponentsLink opens in a new window, AirbusLink opens in a new window, HarwinLink opens in a new window,

Manufacture: University of Warwick, Engineering Technicians.

WUSAT-1 Background

Following six years of working on an ESA Satellite (ESMOLink opens in a new window) with prime contractor Surrey Satellite Technology LtdLink opens in a new window we had completed an enormous learning curve and had considerable experience of satellite design and the Space Systems Engineering process at the highest level.

However, we were now on our own for the first time and a decision was made to concentrate on the rapidly emerging technology of CubeSatLink opens in a new window platforms as an achievable goal for a university team.

Mission Objectives

To study and implement the CubeSat SpecificationLink opens in a new window required for future CubeSat designs for conventional launch and operation.
To apply European Cooperation for Space Standardization (ECSS) standards in order meet potential ESA Review requirements for future missions.
To determine a Modified Space Systems Engineering Methodology for University-based CubeSat MissionsLink opens in a new window that will determine our future design/review procedure.
To design, prototype, build, test, launch and operate a single unit (1U) prototype CubeSat for high-altitude balloon launch. Payload functions to include,
- sensing of ambient temperature, altitude - for internal SD card storage & recovery.
- location tracking system with transmission to ground.
- General Image and video camera recoding for promotional use - via post operation recovery