An aircraft safety system includes impact energy reduction systems including: an aircraft parachute, at least one rotor configured for autorotation, and an energy absorbing system. An automatic control system uses data from speed and altitude sensors to selectively and sequentially deploy the impact energy reduction systems depending on the portion of the aircraft speed and altitude flight envelope in which the aircraft is operating when an emergency is detected.

An aircraft safety system includes impact energy reduction systems including: an aircraft parachute, at least one rotor configured for autorotation, and an energy absorbing system. An automatic control system uses data from speed and altitude sensors to selectively and sequentially deploy the impact energy reduction systems depending on the portion of the aircraft speed and altitude flight envelope in which the aircraft is operating when an emergency is detected.

Disclosed is a coupling system for coupling a piece of equipment rigidly connected to a user with at least one rigging strand, including a central body made of two parts configured to be assembled with one another via an attachment unit, a fastener including two ends, a shell configured to at least partially cover the side surface of the central body, and at least one lock configured to engage with the shell in order to releasably lock the second end of the fastener, the shell being movable in translation over the side surface of the central body and being connected to the central body via at least one elastic recall component.

Disclosed is a coupling system for coupling a piece of equipment rigidly connected to a user with at least one rigging strand, including a central body made of two parts configured to be assembled with one another via an attachment unit, a fastener including two ends, a shell configured to at least partially cover the side surface of the central body, and at least one lock configured to engage with the shell in order to releasably lock the second end of the fastener, the shell being movable in translation over the side surface of the central body and being connected to the central body via at least one elastic recall component.

A hang glider control device may include a cross bar having a first end, a second end, a central region, a first central arm, and a second central arm. The first central arm and the second central arm may be coupled opposingly to the central region. The first end may be formed by a portion of the first central arm distal to the central region, and the second end may be formed by a portion of the second central arm distal to the central region. The first end of the cross bar may be configured to couple the cross bar to the first upright above the base tube, and the second end of the cross bar may be configured to couple the cross bar to the second upright above the base tube so that the crossbar may be generally parallel to the base tube.

A preferred break point is provided in the airframe, where there is a ballistic parachute system which includes a rocket which sits in a rocket canister and a canopy which sits in a canopy canister. The airframe includes a composite material and covers the ballistic parachute system. The preferred break point is located in the airframe over the opening of the rocket canister. A preferred break path is provided in the airframe located at least partially over the opening of the rocket canister and at least partially over the opening of the canopy canister.

Disclosed is a coupling system for coupling a piece of equipment rigidly connected to a user with at least one rigging strand, including a central body made of two parts configured to be assembled with one another via an attachment unit, a fastener including two ends, a shell configured to at least partially cover the side surface of the central body, and at least one lock configured to engage with the shell in order to releasably lock the second end of the fastener, the shell being movable in translation over the side surface of the central body and being connected to the central body via at least one elastic recall component.

A preferred break point is provided in the airframe, where there is a ballistic parachute system which includes a rocket which sits in a rocket canister and a canopy which sits in a canopy canister. The airframe includes a composite material and covers the ballistic parachute system. The preferred break point is located in the airframe over the opening of the rocket canister. A preferred break path is provided in the airframe located at least partially over the opening of the rocket canister and at least partially over the opening of the canopy canister.

The present disclosure discloses a landing aid for a parachutist, in particular for a tandem jump or landing with heavy equipment, having an air bag, which protects the parachutist during landing, wherein the air bag has an inflow opening through which air can flow into the air bag in order to fill it by means of the airstream. It is provided that the landing aid comprises a spring element, by means of which the inflow opening is held in the correct position with respect to the air flow and/or an unpacking process of the air bag is supported.

A hang glider control device may include a cross bar having a first end, a second end, a central region, a first central arm, and a second central arm. The first central arm and the second central arm may be coupled opposingly to the central region. The first end may be formed by a portion of the first central arm distal to the central region, and the second end may be formed by a portion of the second central arm distal to the central region. The first end of the cross bar may be configured to couple the cross bar to the first upright above the base tube, and the second end of the cross bar may be configured to couple the cross bar to the second upright above the base tube so that the crossbar may be generally parallel to the base tube.