An inflatable head restraint system for a parachute assembly may comprise an inflatable volume configured to inflate in response to a deployment of the parachute assembly. The inflatable volume may be located between a left shoulder riser and a right shoulder riser of the parachute assembly. A conduit may be fluidly coupled to the inflatable volume.

An inflatable head restraint system for a parachute assembly may comprise an inflatable volume configured to inflate in response to a deployment of the parachute assembly. The inflatable volume may be located between a left shoulder riser and a right shoulder riser of the parachute assembly. A conduit may be fluidly coupled to the inflatable volume.

A parachute assembly for decelerating an occupant of an ejection seat may comprise a left shoulder riser configured to be located over a left shoulder of the occupant upon deployment of the parachute assembly. A right shoulder riser may be configured to be located over a right shoulder of the occupant upon deployment of the parachute assembly. A head restraint, configured to be behind a head of the occupant upon deployment of the parachute assembly, may be located between the left and right shoulder risers.

A parachute assembly for decelerating an occupant of an ejection seat may comprise a left shoulder riser configured to be located over a left shoulder of the occupant upon deployment of the parachute assembly. A right shoulder riser may be configured to be located over a right shoulder of the occupant upon deployment of the parachute assembly. A head restraint, configured to be behind a head of the occupant upon deployment of the parachute assembly, may be located between the left and right shoulder risers.

A parachute assembly for an ejection seat may comprise a canopy and a first suspension line coupled to the canopy. A first riser may be coupled to the first suspension line. A seat cushion may be coupled to the first riser. The seat cushion may be configured detach from the ejection seat and restrict rearward translation of a head of an occupant of the ejection seat upon deployment of the parachute assembly.

A parachute assembly for an ejection seat may comprise a canopy and a first suspension line coupled to the canopy. A first riser may be coupled to the first suspension line. A seat cushion may be coupled to the first riser. The seat cushion may be configured detach from the ejection seat and restrict rearward translation of a head of an occupant of the ejection seat upon deployment of the parachute assembly.

A device to orient a riser of a parachute. The device can include a twist body that is includes a slot through which the riser passes. The slot includes a twist to change the orientation of the riser from a relatively high-profile orientation to a relatively low-profile orientation. The device can also include a link to connect the riser to the suspension lines on the canopy.

A device to orient a riser of a parachute. The device can include a twist body that is includes a slot through which the riser passes. The slot includes a twist to change the orientation of the riser from a relatively high-profile orientation to a relatively low-profile orientation. The device can also include a link to connect the riser to the suspension lines on the canopy.

A cargo harness comprising a first diagonal strap, a second diagonal strap overlapping the first diagonal strap at a X-crossing. The first diagonal strap may be coupled to the second diagonal strap at a first joint. The cargo harness may also include a cross strap having a first end, a second end and a sleeve disposed between the first end and the second end, wherein the first diagonal strap and the second diagonal strap pass through the sleeve and the sleeve overlaps at least a portion of the x-crossing. In one embodiment, the cargo harness may include a dual-point release strap assembly operably connected to the first and second diagonal strap for connecting a cargo load to a parachute harness.

A cargo harness comprising a first diagonal strap, a second diagonal strap overlapping the first diagonal strap at a X-crossing. The first diagonal strap may be coupled to the second diagonal strap at a first joint. The cargo harness may also include a cross strap having a first end, a second end and a sleeve disposed between the first end and the second end, wherein the first diagonal strap and the second diagonal strap pass through the sleeve and the sleeve overlaps at least a portion of the x-crossing. In one embodiment, the cargo harness may include a dual-point release strap assembly operably connected to the first and second diagonal strap for connecting a cargo load to a parachute harness.