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WUSAT-2 CubeSat Mission

WUSAT-2 Modified 1U Platform

1U CubeSat + Ejection Module on Launch Vehicle

WUSAT-2 CubeSat

Years of Operation: 2013 - 2015

Client: Prof Don Pollacco, 糖心TV Physics

Mission: 1U CubeSat carrying a light spectrometer payload to estimate the density of certain gasses in the Earth's upper atmosphere. Experimental data to be returned via radio transmission system, customised to cope with high-speed (~Mach 2) returning Spacecraft in upper atmosphere.

ESA Mission Codename: - WUSAT-SOLSPEC

Partners:

  • European Space Agency (ESA Academy),
  • German Space Agency DLR (via ),
  • Swedish Space Corporation,
  • Company Partners:

WUSAT-2 Background

WUSAT-2 was designed as a non-standard 1U CubeSat to meet the requirements set by our client, Prof. Don Pollacco, who proposed the concept of a CubeSat that could estimate the density of critical gases (e.g Na and O2) in the Earth's upper atmosphere. This would be achieved by the WUSAT-2 light spectrometer payload, sampling filtered light frequencies during entry into the atmosphere of a planet and estimating the density of each gas at specific altitudes. The presence of such gasses can allow an assessment of a planet's evolutionary history, and would demonstrate that similar CubeSats could be released by a Spacecraft visiting a planet in order to carryout such an investigation. Note: WUSAT-2 is a non-standard CubeSat because the light sensor domes on two external sides of the CubeSat (see above) do not meet CubeSat specification standards, hence, a customised ejection module (above) also had to be produced in order to launch WUSAT-2 from the REXUS launch rocket.

WUSAT-2 ESA Mission Badge

Mission Objectives

  • To design, manufacture, test, launch and operate a CubeSat via approved ESA Space Systems Engineering methodology standards and to meet client payload needs.
  • To successfully complete all European Space Agency phase review requirements
  • In operation - to establish contact with a ground station via a communications link customised to cope with transmission during atmospheric re-entry conditions.
  • To record and estimate atmospheric levels of Na and O2 gasses in Earth's upper atmosphere.

Mission Outcomes

  • To successfully apply a rigorous Space Systems Engineering approach to the development of WUSAT-2 and to meet approval for all up to and including launch.
  • To work with, and meet the requirements of, multiple partners across Europe.
  • To achieve a successful launch and operation of WUSAT-2 including the recovery of payload data via customised radio link during a high-speed (~Mach2) transition in Earth's upper atmosphere. (At the time, the first successful operation of an ejected unit from a REXUS launch in 17 such launches!)
  • To understand and apply other important Space standards required to gain ESA approval for review stages

WUSAT-2 Team 1 2013-14

L-R: Oli Beard, Oliver Vavasour, CJ Hanbury-Williams, Levs Kodners, Matti Konsala, Sarah Iddles, Jess Lomath, Dr Bill Crofts

2013-14 Team Achievements

WUSAT-2 Team 2 2014-15

L-R: Dr Bill Crofts, Matt Havard, Izzy Ferguson, Frank Austin, Francis Eckersley-Carr, Sam Tucker-Harvey, Dom Burr, (inset - Rich Gold).

2014-15 Team Achievements

  • Successfully completed later stage phase reviews including some very extensive re-design/manufacture to obtain ESA approval.
  • Completed final phase approval to obtain WUSAT-2's 'flight ticket' for launch.
  • Spent two weeks at the Sweden Space Centre (ESRANGE) in order to complete launch and obtain operational data.
  • Produced and presented a conference paper WUSAT-SOLSPEC REXUS 17 EXPERIMENT: MEASURING ATMOSPHERIC QUANTITIES OF OXYGEN AND SODIUM; Proc. '22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research', Tromso, Norway, 7 - 12 June 2015 (ESA SP-730, Sept 2015)
  • 2014-15 WUSAT-2 Final PresentationLink opens in a new window
  • 2014-15 WUSAT-2 Technical ReportLink opens in a new window

WUSAT-2 The Movie (2015) - approx 10 mins

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