PROPELLANT AND PROCESS FOR PRODUCING A PROPELLANT
    2.
    发明申请
    PROPELLANT AND PROCESS FOR PRODUCING A PROPELLANT 有权
    用于生产推进剂的推进剂和方法

    公开(公告)号:US20110284140A1

    公开(公告)日:2011-11-24

    申请号:US13110158

    申请日:2011-05-18

    摘要: A propellant for guns includes at least one energy carrier, nitrocellulose and cellulose acetate butyrate. At least part of the nitrocellulose is alcohol-soluble nitrocellulose. The nitrocellulose serves as a binder and for that purpose is present in a concentration of at least 15% by weight in the propellant. A process for producing a propellant is also provided.

    摘要翻译: 用于枪支的推进剂包括至少一种能量载体,硝酸纤维素和乙酸丁酸纤维素。 硝酸纤维素的至少一部分是醇溶性硝酸纤维素。 硝酸纤维素用作粘合剂,为此目的在推进剂中以至少15重量%的浓度存在。 还提供了一种生产推进剂的方法。

    Infra-Red Decoy Flare
    3.
    发明申请
    Infra-Red Decoy Flare 审中-公开
    红外诱饵耀斑

    公开(公告)号:US20090120545A1

    公开(公告)日:2009-05-14

    申请号:US11988170

    申请日:2006-06-07

    摘要: The invention provides an infra-red decoy flare comprising a pyrotechnic composition which comprises an extrudable and energetic binder in an amount in the range of from 4-35 wt %, which binder comprises a nitrocellulose, an oxidator in an amount in the range of from 40-80 wt %, a pyrotechnic fuel in an amount in the range of from 15-35 wt %, and a carbon source in an amount of up to and including 10 wt %, all amounts based on total pyrotechnic composition. The invention further provides a process for preparing said infra-red decoy flare.

    摘要翻译: 本发明提供了一种红外诱饵火炬,其包括烟火组合物,该烟火组合物包含4-35重量%范围内的可挤压和高能粘合剂,所述粘合剂包含硝化纤维素,氧化剂的量范围为 40-80重量%,15-35重量%范围内的烟火燃料和至多并且包括10重量%的量的碳源,基于总烟火组合物的所有量。 本发明还提供了制备所述红外诱饵火炬的方法。

    Propellant composition containing beryllium hydride, nitrocellulose and nitrate co-plasticizers
    8.
    发明授权
    Propellant composition containing beryllium hydride, nitrocellulose and nitrate co-plasticizers 失效
    含有氢氧化铵,硝酸纤维素和硝酸盐共增塑剂的丙烯酸酯组合物

    公开(公告)号:US3861970A

    公开(公告)日:1975-01-21

    申请号:US74083468

    申请日:1968-06-25

    申请人: US AIR FORCE

    IPC分类号: C06B25/22 C06B27/00 C06D5/06

    CPC分类号: C06B25/22 C06B27/00

    摘要: A composite, double-base, solid rocket propellant composition which utilizes beryllium hydride as a high energy fuel in combination with a nitro-nitrate ester plasticizer. The particular ester plasticizer used in the propellant composition serves to produce the high non-equilibrium flame temperatures needed for attaining high beryllium hydride combustion efficiencies.

    摘要翻译: 一种复合的双基固体火箭推进剂组合物,其使用氢化铍作为高能燃料与硝基硝酸酯增塑剂的组合。 用于推进剂组合物中的特定酯增塑剂用于产生获得高铍氢化物燃烧效率所需的高非平衡火焰温度。