{"title":"SUU-25F/A分配器吊舱在F/A- 18a飞机上的飞行测试程序","authors":"D. Roberts","doi":"10.1109/AERO.2001.931222","DOIUrl":null,"url":null,"abstract":"A modified SUU-25F/A dispenser pod system was evaluated for employment on the U.S. Navy F/A-18A Hornet fighter/attack aircraft. Testing had been conducted previously on the F/A-18A with a standard SUU-25F/A system, but was discontinued when the dispensed stores nearly collided with the horizontal stabilator. A modified system of two pods on the outboard wing station was designed to increase the separation clearance of the aft launched stores, below and outboard of the horizontal stabilator. Test methodology included a level flight build-up in airspeed with qualitative analysis of separation characteristics being conducted real-time using onboard telemetered video. The innovations implemented in this program enabled demonstration of store safe separation with a minimum number of test flights and store expenditures.","PeriodicalId":329225,"journal":{"name":"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)","volume":"33 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2001-03-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"SUU-25F/A dispenser pod flight test program on the F/A-18A aircraft\",\"authors\":\"D. Roberts\",\"doi\":\"10.1109/AERO.2001.931222\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A modified SUU-25F/A dispenser pod system was evaluated for employment on the U.S. Navy F/A-18A Hornet fighter/attack aircraft. Testing had been conducted previously on the F/A-18A with a standard SUU-25F/A system, but was discontinued when the dispensed stores nearly collided with the horizontal stabilator. A modified system of two pods on the outboard wing station was designed to increase the separation clearance of the aft launched stores, below and outboard of the horizontal stabilator. Test methodology included a level flight build-up in airspeed with qualitative analysis of separation characteristics being conducted real-time using onboard telemetered video. The innovations implemented in this program enabled demonstration of store safe separation with a minimum number of test flights and store expenditures.\",\"PeriodicalId\":329225,\"journal\":{\"name\":\"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)\",\"volume\":\"33 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2001-03-10\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO.2001.931222\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO.2001.931222","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
摘要
一种改进的SUU-25F/A分配吊舱系统被评估用于美国海军F/A- 18a大黄蜂战斗机/攻击机。先前在F/ a - 18a上使用标准的SUU-25F/ a系统进行了测试,但由于分配的支架几乎与水平稳定器相撞而中断。设计了一个由外翼站的两个吊舱组成的改进系统,以增加尾部发射的储存库、水平稳定器的下方和外侧的分离间隙。测试方法包括利用机载遥测视频对分离特性进行实时定性分析,并在空速上进行水平飞行。在该计划中实施的创新以最少的试飞次数和最少的存储支出实现了存储安全分离的演示。
SUU-25F/A dispenser pod flight test program on the F/A-18A aircraft
A modified SUU-25F/A dispenser pod system was evaluated for employment on the U.S. Navy F/A-18A Hornet fighter/attack aircraft. Testing had been conducted previously on the F/A-18A with a standard SUU-25F/A system, but was discontinued when the dispensed stores nearly collided with the horizontal stabilator. A modified system of two pods on the outboard wing station was designed to increase the separation clearance of the aft launched stores, below and outboard of the horizontal stabilator. Test methodology included a level flight build-up in airspeed with qualitative analysis of separation characteristics being conducted real-time using onboard telemetered video. The innovations implemented in this program enabled demonstration of store safe separation with a minimum number of test flights and store expenditures.