000022849 001__ 22849
000022849 005__ 20220110134530.0
000022849 04107 $$aeng
000022849 046__ $$k2018-05-14
000022849 100__ $$aPejchar, J.
000022849 24500 $$aModern methods of parachute rescue system testing

000022849 24630 $$n24.$$pEngineering Mechanics 2018
000022849 260__ $$bInstitute of Theoretical and Applied Mechanics of the Cech Academy of Sciences, Prague
000022849 506__ $$arestricted
000022849 520__ $$2eng$$aThis paper presents an improved free-flight testing method applicable to parachute systems used by rescue systems. The method as described allows parachute testing in the speeds and for payloads over the limits acceptable for available testing platforms. Based on an algorithm with the approach for achieving demanded speed, it also includes a design of instrumented parachute testing vehicle. Both methods with the algorithm and testing vehicle were evaluated by airdrop tests and their features have been successfully proved..

000022849 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000022849 653__ $$aparachute, rescue system, testing

000022849 7112_ $$aEngineering Mechanics 2018$$cSvratka, CZ$$d2018-05-14 / 2018-05-17$$gEM2018
000022849 720__ $$aPejchar, J.$$iHájek, T.
000022849 8560_ $$ffischerc@itam.cas.cz
000022849 8564_ $$s347669$$uhttps://invenio.itam.cas.cz/record/22849/files/665.pdf$$yOriginal version of the author's contribution in proceedings, page , section KIN.
000022849 962__ $$r21225
000022849 980__ $$aPAPER