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１９６２～１９７８年间，美国霍普金斯大学应用物理实验室开发了用于舰队防御的导弹技术。研制工作始于两种导弹构型的初步设计和为水面舰队提供防御所期望性能的计算。设计了一系列新型固定形状的多模块超音速进气道，制作了风洞模型并在最大攻角为１５°、Ｍａ＝４～１０状态下对其进行了试验。在直连式试验装置中进行了喷嘴和燃烧室试验。研制并试验了包括硼烷和烷基铝在内的多种可储存的活性液体燃料。开发了多种新的试验技术和检测装置。该计划完成了全尺寸发动机在Ｍａ＝５～７．３的自由射流状态下的试验，并完成了一系列导弹构型设计。
From 1962 to 1978, Hopkins Applied Physics Laboratory developed a missile technology for fleet defense. Development began with the initial design of the two missile configurations and the calculation of the desired performance of the surface fleet in defense. A series of new fixed-shape multi-module supersonic gas inlets were designed and a wind tunnel model was fabricated and tested at a maximum angle of attack of 15 ° and Ma = 4 ~ 10. Nozzles and combustor tests were performed in direct-coupled test setups. A variety of storable active liquid fuels including boranes and aluminum alkyls have been developed and tested. A number of new test technologies and testing devices have been developed. The program completed a full-scale engine test at a free jet with Ma = 5 to 7.3 and completed a series of missile configuration designs.