A device includes a harness system configured to be attached to a parachute harness of a parachute. The device also includes a propulsion system connected to the harness system, wherein the propulsion system is configured to be off when undeployed and during freefall, and wherein the propulsion system is configured to deploy during canopy flight stage to generate thrust for a parachutist of the parachute. The device further includes a circuitry configured to control power generation by the propulsion system to control the thrust. The device includes a power source configured to power the circuitry and the propulsion system.
PARACHUTE RANGE AUGMENTER
2024-09-26
Patent
Electronic Resource
English
IuD Bahn | 2010
Augmenter la vitesse commerciale
IuD Bahn | 1998
Jet-Engine Test Cell Augmenter Performance
AIAA | 1998
|Jet-Engine Test Cell Augmenter Performance
Online Contents | 1998
|