Solid rocket propellant
    1.
    发明授权
    Solid rocket propellant 有权
    固体火箭推进剂

    公开(公告)号:US06066214A

    公开(公告)日:2000-05-23

    申请号:US183750

    申请日:1998-10-30

    IPC分类号: C06B45/10

    CPC分类号: C06B45/10

    摘要: A solid propellant composition includes an oxidizer, a fuel and a binder, the oxidizer containing a significant amount of bismuth oxide (Bi.sub.2 O.sub.3)

    摘要翻译: 固体推进剂组合物包括氧化剂,燃料和粘合剂,氧化剂含有大量的氧化铋(Bi 2 O 3)

    Cross-linked double base propellant having improved low temperature
mechanical properties
    2.
    发明授权
    Cross-linked double base propellant having improved low temperature mechanical properties 失效
    具有改进的低温机械性能的交联双基推进剂

    公开(公告)号:US4659402A

    公开(公告)日:1987-04-21

    申请号:US860422

    申请日:1977-12-14

    CPC分类号: C06B45/10 C06B25/30 C06B25/34

    摘要: Cross-linked double base propellants having improved low temperature mechanical properties are provided. The improved properties are achieved by using a mixture of polyglycoladipate and polycaprolactone as the binder prepolymer and employing a lacquer grade nitrocellulose containing 12.1% N to 12.6% N as the source of nitrocellulose.

    摘要翻译: 提供具有改进的低温机械性能的交联双基推进剂。 通过使用聚乙二醇脂肪酸酯和聚己内酯的混合物作为粘合剂预聚物并使用含有12.1%N至12.6%N作为硝化纤维素来源的漆级硝酸纤维素来实现改进的性能。

    Composite double base propellant composition containing ferric fluoride
    3.
    发明授权
    Composite double base propellant composition containing ferric fluoride 失效
    含氟化铁的复合双基推进剂组合物

    公开(公告)号:US3954531A

    公开(公告)日:1976-05-04

    申请号:US370585

    申请日:1973-06-14

    IPC分类号: C06B23/00 C06B33/08

    CPC分类号: C06B23/007

    摘要: Composite-modified double base propellants containing aluminum as a metal el having ferric fluoride added as a combustion catalyst, a thermal stabilizer and an aid in reducing exhaust plume interference with a radar guidance system.

    摘要翻译: 含有作为燃料催化剂添加了氟化铁的铝作为金属燃料的复合改性双基推进剂,热稳定剂和有助于减少与雷达引导系统的排气羽流干扰。