FIELD: transport.
SUBSTANCE: invention relates to aircraft, specifically to devices for dropping or detaching a payload from aircraft. Device consists of transporter-launcher container secured on structural elements along SC fuselage. The container is provided with window at rear butt end for payload passing through. Payload is placed on at least two guides with creation of pneumatic chamber in front part of container interior. The payload is attached to container by fastener made with possibility of fastener release. Fastener release system includes high-pressure gas source provided with electrically operated drive, and drop control system. The device is equipped with at least payload partial exit signalling device and at least one high-temperature gas jet source with launcher.
EFFECT: reduced time of payload dropping without increasing container weight and maximum longitudinal acceleration.
1 dwg
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Authors
Dates
2014-11-20—Published
2012-09-20—Filed