http://www.cnr.it/ontology/cnr/individuo/prodotto/ID234426
WATER IMPACT EXPERIMENTS ON A SCALED IXV MODEL (Contributo in atti di convegno)
- Type
- Label
- WATER IMPACT EXPERIMENTS ON A SCALED IXV MODEL (Contributo in atti di convegno) (literal)
- Anno
- 2012-01-01T00:00:00+01:00 (literal)
- Alternative label
A. Iafrati^1, F. La Gala^1, M. Miozzi^1, G. Di Vita^2 (2012)
WATER IMPACT EXPERIMENTS ON A SCALED IXV MODEL
in 12th European Conference on Spacecraft Structures, Materials & Environmental Testing, NoordWijk (NL), 20-23 Marzo 2012
(literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#autori
- A. Iafrati^1, F. La Gala^1, M. Miozzi^1, G. Di Vita^2 (literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#titoloVolume
- Proceedings of the 12th European Conference on Spacecraft Structures, Materials & Environmental Testing (literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#pagineTotali
- Note
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#affiliazioni
- ^1 CNR-INSEAN, ^2 ESA - Paris (literal)
- Titolo
- WATER IMPACT EXPERIMENTS ON A SCALED IXV MODEL (literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#isbn
- 978-92-9092-255-1 (literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#curatoriVolume
- Abstract
- The results of an experimental campaign of the splashdown of the ESA IXV aimed at supporting the numerical simulations of the problem are presented here. Tests were
done at different attitudes with and without wind effects. Measurements involved accelerations and angular velocities obtained from an Inertial Measurement Unit (IMU),
pressures and dynamic accelerations. The loads acting on the flaps were also measured through the instrumentation of the body flap connection elements. All signals were
transmitted via a Bluetooth connection, thus avoiding the spurious effects of umbilical cables. Measurements were supported by 100 Hz videos of the entry process. Attention
is here focused on the description of the experimental setup and on the discussion of some of the most relevant results obtained in terms of the rigid body motion and
forces acting on the flaps. (literal)
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