| 摘要 |
An infrared (IR) decoy flare for a helicopter, or an aircraft with a similar size engine, the flare including a casing, at least two longitudinal flare pellets in the casing, a single impulse cartridge to serially expel and ignite the pellets, and a delay element associated with at least one of the flare pellets and arranged to be ignited by the impulse cartridge and to expel the associated flare pellet a predetermined interval after ignition.
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