首页> 外文会议>56th International Astronautical Congress 2005 vol.10 >French solid motors for missiles and rockets from WWII to the Sixties
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French solid motors for missiles and rockets from WWII to the Sixties

机译:第二次世界大战至60年代的法国用于导弹和火箭的固体发动机

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At the beginning of research on solid propulsion, France had a peculiar organization because of the state monopoly on the production of gun powders existing at that time: Direction des Poudres was responsible for the energetic part of the solid motor and supplied private companies or government agencies with grains. Before World War II, some industrial capacity in the field of extruded double base (EDB) propellant for guns did exist at Direction des Poudres. After the war, EDB propellants (SD grains) were soon developed and used on small diameter missiles. Cast double base propellant (CDB) development started in 1950. This family (Epictete grains) allowed higher sizes, compatible with all types of tactical missiles. Shortly afterwards the first French composite propellant (Plastorgol grains) appeared, using PVC binder. During the 1950's, several rocket vehicle programs using these propellants were developed, particularly a series of long range anti-aircraft missiles. The motors developed for these missiles gave birth to several families of test rockets and sounding rockets (ONERA, SEREB, Sud Aviation,...).rnIn 1959, the decision to develop a deterrent force mainly based on the use of ballistic missiles deeply reoriented the French rocket industry. Created in order to manage the development of the ballistic missiles, SEREB initiated a program of basic ballistic studies. This program began with vehicles using available 55 cm and 80 cm Plastorgol solid motors. It continued with liquid rockets and also solids using a new propellant (Isorgol grains) based on polyurethane binder. The most powerful of these vehicles (the Precious Stones series) was Saphir, constituted by an Emeraude liquid stage topped by a solid Topaze. In December 1961, three months before the official creation of CNES, it was decided to develop a space launcher, named Diamant by replacing the Saphir payload by a third stage. This new upper stage was tested atop a reliable Plastorgol-based rocket, forming the Rubis 2-stage vehicle, before the maiden - and successful -launch of Diamant in November 1965.rnThis paper presents the evolution of the French solid propulsion during this period (up to 80 cm in diameter) by describing the main applications in the field of missiles and their adaptation to the domain of the sounding rockets and space launchers.
机译:在固体推进研究之初,法国成立了一个特殊的组织,因为当时国家垄断了当时生产的火药粉末的生产:Directory des Poudres负责固体电动机的高能部分,并向私人公司或政府机构提供产品与谷物。第二次世界大战之前,Directory des Poudres确实在枪支用挤压双基(EDB)推进剂领域具有一定的工业能力。战后,EDB推进剂(SD颗粒)很快得到开发,并用于小直径导弹。铸造双基推进剂(CDB)的开发始于1950年。该系列(Epictete谷物)允许更大的尺寸,与所有类型的战术导弹兼容。此后不久,出现了第一批使用PVC粘合剂的法国复合推进剂(Plastorgol颗粒)。在1950年代,开发了几种使用这些推进剂的火箭飞行器程序,特别是一系列远程防空导弹。为这些导弹开发的电动机催生了数个试验火箭和探空火箭系列(ONERA,SEREB,Sud Aviation等)。1959年,决定主要基于深度改编的弹道导弹来发展威慑力量的决定。法国火箭工业。为了管理弹道导弹的发展而创建的SEREB发起了一项基础弹道研究计划。该程序从使用55厘米和80厘米Plastorgol固体发动机的车辆开始。它继续使用液体火箭,并使用基于聚氨酯粘合剂的新型推进剂(艾索尔谷粒)进行固体处理。这些车辆中功能最强大的(宝石系列)是Saphir,由Emeraude液位和固体Topaze组成。 1961年12月,也就是正式成立CNES的三个月前,决定研发一种名为Diamant的太空发射器,将第三阶段的Saphir载荷替换掉。在1965年11月Diamant首次并成功发射前,这种新的上层级在可靠的基于Plastorgol的火箭上进行了测试,形成了Rubis 2级运载工具.rn本文介绍了法国在此期间的固体推进力的演变(直径不超过80厘米)描述了导弹领域的主要应用及其对探测火箭和太空发射器领域的适应性。

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