Two-stage hydrazine rocket motor
    1.
    发明授权
    Two-stage hydrazine rocket motor 失效
    两级液压油马达

    公开(公告)号:US3695041A

    公开(公告)日:1972-10-03

    申请号:US3695041D

    申请日:1970-05-08

    IPC分类号: C06B47/08 F02K9/08 F02K3/04

    CPC分类号: F02K9/08 C06B47/08

    摘要: Hydrazine is catalytically decomposed in a primary reaction chamber. During low thrust operation all of the decomposition products flow directly to the nozzle. During high thrust operation an oxidizer is reacted with a major portion of the decomposed hydrazine in the central portion of the secondary reaction chamber downstream of the primary reaction chamber. The remaining decomposed hydrazine is directed as a buffer layer along the inner surface of the secondary reaction chamber''s outer wall, to serve as a coolant.

    摘要翻译: 肼在一级反应室中催化分解。 在低推力运行期间,所有的分解产物直接流到喷嘴。 在高推力操作期间,氧化剂与主反应室下游的次级反应室的中心部分中的大部分分解的肼反应。 剩余的分解的肼沿着二次反应室的外壁的内表面作为缓冲层引导,用作冷却剂。