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LATERAL DISPENSE OF INFRARED (IR) DECOYS FROM THE F-16PYLON INTEGRATED DISPENSER SYSTEM (PIDS)

机译:F-16PYLON集成分配器系统(PIDS)的红外(IR)诱饵的横向分配

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The outboard dispense of MJU-50/B infrared decoys from the PIDS pylon on an F-16 aircraftrnwith wingtip AIM-9J missile shapes was demonstrated in flight. The flight test demonstrationrnwas performed to investigate the compatibility of outboard dispensed infrared decoy materialrncontact with the aircraft wing surfaces, wingtip missiles and launchers. Since store separationrnflight test missions are typically designed to avoid collisions between the separated store andrnthe aircraft or captive stores, the unique considerations that arose from planningrncountermeasure dispense missions with intended collisions are discussed. To providernconditions favorable for decoy contact with the aircraft and AIM-9J missile, the decoys wererndispensed during level rolling maneuvers into the decoy dispense plane at low to moderaternairspeeds. Impact with the aircraft wing surface was incidental, but substantial decoy materialrnimpacted the AIM-9J tail fins at all airspeeds tested. The data presented include the dispensernflight conditions, pre-flight, in-flight, and post-flight photographs, and select high-speed filmrnsequences from onboard cameras. The paper addresses the investigation of the flight regime,rnthe determination of appropriate flight restrictions, and includes recommendations for furtherrnflight testing to characterize the outboard dispense of MJU-50/B infrared decoys fromrnoperational F-16 configurations.
机译:在飞行中演示了从FIDS机翼上的PIDS吊塔向外侧分配MJU-50 / B红外诱饵的过程。进行了飞行试验演示,以研究外侧分配的红外诱饵材料与飞机机翼表面,翼尖导弹和发射器的接触性。由于商店分离飞行测试任务通常被设计为避免分离的商店与飞机或俘虏商店之间发生碰撞,因此讨论了计划对策分配任务与预期碰撞的独特考虑。为了提供有利于诱饵与飞机和AIM-9J导弹接触的条件,诱饵是在低速至中速空投水平飞行时进入诱饵分配飞机的。偶然接触飞机机翼表面,但是在所有测试的空速下,大量诱饵材料影响了AIM-9J尾鳍。呈现的数据包括点胶机飞行条件,飞行前,飞行中和飞行后的照片,以及从机载相机中选择高速胶卷序列。本文着重研究飞行状态,确定适当的飞行限制,并包括进一步飞行测试的建议,以表征F-16构型的MJU-50 / B红外诱饵的舷外分配。

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