The use of "NIRVANA" facility for balloon characterization: strain and tightness measurements of zero pressure and superpressure balloon subsystems

Details The use of "NIRVANA" facility for balloon characterization: strain and tightness measurements of zero pressure and superpressure balloon subsystems The use of "NIRVANA" facility for balloon characterization: strain and tightness measurements of zero pressure and superpressure balloon subsystems

Aug 2003

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003esasp.530..207s&link_type=abstract

In: 16th ESA Symposium on European Rocket and Balloon Programmes and Related Research, 2 - 5 June 2003, Sankt Gallen, Switzerlan

Physics

Space Flight: Techniques, Instrumentation, Ranges

Scientific paper

The NIRVANA facility, set in the Space Environment Department of ONERA-Toulouse, has been developed., by CNES funds, in order to study, in realistic consitions (temperature, absolute and differential pressures, preloading and loading time), the tightness and the mechanical behavior of zero-pressure and super-pressure balloon subsystems like film envelopes, assemblies or apex parts.

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