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Propellants gas-generating

Gas Cannon Device, patented by Peake in 1934(Ref), was claimed to be an improvement for previously proposed "gas cannons . The object of this device was to provide a gas generating propellant in measured form. [Pg.659]

Ammonium nitrate (AN) imparts slower burn rates but is a high gas producer and accordingly is used for gas generator propellants. AN has an oxygen balance 20%,... [Pg.235]

R.AH. Strecker H.S. Haiss, Solid 5-Aminotetrazole Nitrate Gas Generating Propellant with Block Copolymer Binder , USP 3898112 (1975) ... [Pg.614]

Strontium nitrate is used in pyrotechnics as a flame-coloring oxidizer for red-colored fireworks. Recently, strontium nitrate is used as oxidizer in gas generating propellants e.g. for airbacks. [Pg.300]

The chemical compositions of the gas-generating propellants for ducted rocket engines are different from those of the propellants used for rocket motors. The physicochemical properties of the gas-generating propellants used for variable flow systems are[12,13]... [Pg.227]

The gas-generating propellants are (1) ammonium perchlorate-polybutadiene (AP-PB) composite propellants, (2) nitrocellulose-nitroglycerin (NC-NG) doublebase propellants, and (3) glycidyl azide polymer (GAP) propellants. [Pg.227]

Typical gas-generating propellants are (1) AP-PB composite propellant composed of 50% AP and 50% HTPB that is cured with isophorone diisocyanate (IPDI), (2) NC-NG double-base propellant composed of 70% NC and 30% NG that is plasticized with diethyl phthalate (DEP), and (3) GAP propellant composed of GAP copolymer that is cured with 12.0% hexamethylene diisocyanate (HMDI) and cross-linked with 3.2 % trimethylolpropane (TM P). [Pg.227]

Figure 9-23. Burning rate characteristics of gas-generating propellants. Figure 9-23. Burning rate characteristics of gas-generating propellants.
Figure 9-25. Adiabatic flame temperature of GAP/B gas-generating propellant as a function of air to fuel ratio. Figure 9-25. Adiabatic flame temperature of GAP/B gas-generating propellant as a function of air to fuel ratio.
See other pages where Propellants gas-generating is mentioned: [Pg.341]    [Pg.392]    [Pg.103]    [Pg.225]    [Pg.524]    [Pg.103]    [Pg.225]    [Pg.529]    [Pg.130]    [Pg.157]    [Pg.1773]    [Pg.151]    [Pg.153]    [Pg.94]    [Pg.194]    [Pg.225]    [Pg.226]    [Pg.227]    [Pg.229]    [Pg.230]    [Pg.231]    [Pg.110]    [Pg.400]    [Pg.170]    [Pg.1213]   
See also in sourсe #XX -- [ Pg.225 ]

See also in sourсe #XX -- [ Pg.225 ]



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