Detail aplikovaného výsledku

Multi stage aerodynamic decelerator system for high speeds

BÁBOVKA, M.; DOROTKA, M.; POPELA, R.; HÁJEK, T.; GRIM, R.

Originální název

Multi stage aerodynamic decelerator system for high speeds

Anglický název

Multi stage aerodynamic decelerator system for high speeds

Druh

Prototyp

Abstrakt

This result is composed of a three stages complex system for GA aircrafts and VTOL vehicles. There is first smaller parachute - first stage - deployed by GBS10 pyrogenerator based system used for deceleration from high cruise speeds up to 350 km/h, second stage medium size parachute for deceleration to speed less than 100 km/h and last stage composed from clustered small parachutes (currently is designed for 36 canopies) for final deceleration.

Abstrakt aglicky

This result is composed of a three stages complex system for GA aircrafts and VTOL vehicles. There is first smaller parachute - first stage - deployed by GBS10 pyrogenerator based system used for deceleration from high cruise speeds up to 350 km/h, second stage medium size parachute for deceleration to speed less than 100 km/h and last stage composed from clustered small parachutes (currently is designed for 36 canopies) for final deceleration.

Klíčová slova

drop test; multi stage activation; high speed rescue

Klíčová slova anglicky

drop test; multi stage activation; high speed rescue

Umístění

LÚ FSI

Licenční poplatek

K využití výsledku jiným subjektem je vždy nutné nabytí licence