Thanks to the high latitude of the location the new scenario of the Svalbard Islands as well as that of the already operative Swedish launch base is very close to becoming a principal launching site for Long Duration Ballooning (LDB) Arctic campaigns. LDB flights, rather than mid latitude flights that last several hours have become a suitable framework for all efforts to create low cost campaigns. The scientific world, which uses balloons to record measurements beyond the atmosphere, needs both frequently scheduled campaigns and an optimized organization capable of reducing flight costs. It is obvious that a reducing of general costs means keeping in mind, during all design phases, versatility and the standardization of common facilities such as gondola frame as well as the protection of the solar panels upon landing etc. The multi-user payload is certainly the first step for reducing launch costs . Each balloon is launched as much as possible when its payload hosts a number of experiments that weight just a little less than its maximum lifting capacity, apart from the necessary their mutual compatibility. A second step, concerns the optimization of the gondola frame design. It must manufacture gondolas easy to assemble, transport and as well as be easy to modify in shape in order to host a different combination of a given number of experiments, once these have been selected by a scientific authority for the same balloon. The new concept in designing platform which takes advantage of special mechanical elements that are capable both of jointing different beam lengths and of distributing tensile or compression stress only is proposed. The gondola can be assembled simply by only cutting structural aluminum beams into different lengths . Differences between traditional rigid structures and the new concept of construction are pointed out, as a reduction in the total weight and as an easy way to balance the gondola almost without adding extra weight. An example of how the new mechanical joint works and how its behavior closely approximates to the theoretical one is also demonstrated. The study is devoted to design the platform of one of the next balloon experiments (funded by ASI): The Large Scale Polarization Explorer (LSPE).

Boscaleri, A., Fiorineschi, L., Rissone, P., Baldi, M., Zannoni, M. (2011). A new approach in designing of stratospheric platforms aimed at multi-user LDB flights. In Proceedings 20th ESA Symposium on European Rocket and Balloon Programmes and Related Research (pp.593-598). ESA Communications.

A new approach in designing of stratospheric platforms aimed at multi-user LDB flights

ZANNONI, MARIO
2011

Abstract

Thanks to the high latitude of the location the new scenario of the Svalbard Islands as well as that of the already operative Swedish launch base is very close to becoming a principal launching site for Long Duration Ballooning (LDB) Arctic campaigns. LDB flights, rather than mid latitude flights that last several hours have become a suitable framework for all efforts to create low cost campaigns. The scientific world, which uses balloons to record measurements beyond the atmosphere, needs both frequently scheduled campaigns and an optimized organization capable of reducing flight costs. It is obvious that a reducing of general costs means keeping in mind, during all design phases, versatility and the standardization of common facilities such as gondola frame as well as the protection of the solar panels upon landing etc. The multi-user payload is certainly the first step for reducing launch costs . Each balloon is launched as much as possible when its payload hosts a number of experiments that weight just a little less than its maximum lifting capacity, apart from the necessary their mutual compatibility. A second step, concerns the optimization of the gondola frame design. It must manufacture gondolas easy to assemble, transport and as well as be easy to modify in shape in order to host a different combination of a given number of experiments, once these have been selected by a scientific authority for the same balloon. The new concept in designing platform which takes advantage of special mechanical elements that are capable both of jointing different beam lengths and of distributing tensile or compression stress only is proposed. The gondola can be assembled simply by only cutting structural aluminum beams into different lengths . Differences between traditional rigid structures and the new concept of construction are pointed out, as a reduction in the total weight and as an easy way to balance the gondola almost without adding extra weight. An example of how the new mechanical joint works and how its behavior closely approximates to the theoretical one is also demonstrated. The study is devoted to design the platform of one of the next balloon experiments (funded by ASI): The Large Scale Polarization Explorer (LSPE).
paper
Practical, Theoretical or Mathematical/ aluminium; atmospheric measuring apparatus; balloons; beams (structures); compressive strength; high altitude stratospheric platforms; tensile strength/ stratospheric platform; multiuser LDB flights; Svalbard Islands; long duration ballooning Arctic campaigns; solar panel protection; gondola frame design; mechanical elements; tensile stress distribution; compression stress distribution; structural aluminum beam; mechanical joint; large scale polarization explorer; maximum lifting capacity/ A9480 Instrumentation and techniques for aeronomy, space physics, and cosmic rays B7710B Atmospheric, ionospheric and magnetospheric techniques and equipment B6250 Radio links and equipment E1710 Engineering materials E2110A General shapes and structures E2180B Plasticity (mechanical engineering)
English
20th ESA Symposium on European Rocket and Balloon Programmes and Related Research
22-26 May 2011
Proceedings 20th ESA Symposium on European Rocket and Balloon Programmes and Related Research
978-92-9092-264-3
2011
593
598
none
Boscaleri, A., Fiorineschi, L., Rissone, P., Baldi, M., Zannoni, M. (2011). A new approach in designing of stratospheric platforms aimed at multi-user LDB flights. In Proceedings 20th ESA Symposium on European Rocket and Balloon Programmes and Related Research (pp.593-598). ESA Communications.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/10281/38933
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