Support climate change research with a cost-effective and re-usable high altitude balloon air sampling system that reduces the current complexities and limitations of obtaining air samples for stratospheric greenhouse gas distribution analysis.
The idea for the experiment stems from concerns over the realities of climate change as a result of human activity coupled with the complexity and limitations of obtaining much needed greenhouse gas profile data to better understand the issue.
The Alternative to AirCore (AAC) sampling system will be launched as a proof-of-concept and its reliability will be validated against the samples collected by a proven AirCore sampling system that will also be part of the payload.
After much brainstorming on what kind of experiment to fly, the team pitches the TUBULAR project to a panel of space industry experts at the European Space Research and Technology Centre (ESTEC) in Noordwijk, Netherlands.
During this phase the experiment objectives will be fixed and a complete preliminary design will be produced. The experiment requirements should be defined in detail, along with a preliminary project and test plan. This Stage culminates in the Preliminary Design Review (PDR), which is held during the Student Training Week. Prior to the PDR, Version 1 of the SED should be submitted. This document will be used to assess the experiment design, and will form the basis of the review.
By this stage the experiment design will have reached a high level of maturity. The experiment requirements should be fixed, and a detailed verification and test plan will have been drafted, along with a well thought out flight plan. Any recommendations or action items identified at PDR will have been addressed and documented. This stage ends with the Critical Design Review (CDR). Again shortly before the CDR, Version 2 of the SED should be submitted for review. Upon successful completion of the CDR the experiment design will be frozen so that it can be manufactured and verified.
Six weeks after the CDR, Version 3 of the SED – containing a final experiment design, project plan and flight plan – should be submitted again prior to an Integration Progress Review (IPR). Following the submission, experts will visit each experiment team to ensure that integration is progressing smoothly, and that any major issues identified at CDR have been closed out. The manufactured experiment and/or individual subsystems should be tested thoroughly at this stage.
Shortly before the launch campaign, the team will undergo an Experiment Acceptance Review (EAR) to ensure that the experiment is flight ready. Version 4 of the SED must be submitted with the results of this review before the experiment is integrated onto the balloon platforms. This document will contain all necessary information required by EuroLaunch for campaign operations. It should incorporate a complete description of the experiment design, as-built, along with the results of the test campaign, and detailed pre and post-flight procedures.
The moment of truth, hold on to your hats! The team finally launches their experiment from Esrange Space Center, Europe's premiere spaceport. Esrange is located in the very north of Sweden, above the Arctic Circle (68°N, 21°E) and has access to a vast, unpopulated impact and recovery area. The facility has been operational since 1966 and is presently used by the international scientific community for launching sounding rockets for microgravity and atmospheric research as well as high altitude balloons for astronomy, atmospheric research and drop tests of space and aerial vehicles.
The fifth and last version of the SED will be submitted after completion of the launch campaign, as a final report. It will represent a complete account of the whole project, and will include all as-built design documentation. The post-flight analysis and results will also be included, along with a summary of all Lessons Learned. The completion of this final report will be required for all members to receive certification of participation in the REXUS/BEXUS programme.
Scientific Division
Scientific Division
Mechanical Division
Mechanical Division
Software Division
Thermal Division
Management Division
Project Manager
Mechanical Division
Electrical Division
Software Division
Electrical Division
Thermal Division