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TAGN-GAP propellant

The burning surface of TAGN-GAP propellants is heterogeneous because of the decomposition of TAGN particles and GAP. In the region of low l(TAGN) (below... [Pg.181]

Fig.4.22 Specific impulse, adiabatic flame temperature, and molecular mass of combustion products for TAGN-GAP composite propellants. Fig.4.22 Specific impulse, adiabatic flame temperature, and molecular mass of combustion products for TAGN-GAP composite propellants.
Fig. 4.23 Mole fractions of combustion products of TAGN-GAP composite propellants. Fig. 4.23 Mole fractions of combustion products of TAGN-GAP composite propellants.
Table 7.7 Physicochemical properties of TAGN-GAP and HMX-GAP propellants composed of cap(0-80)-... Table 7.7 Physicochemical properties of TAGN-GAP and HMX-GAP propellants composed of cap(0-80)-...
Fig. 7.59 Burning rates and temperature sensitivity thereof for TAGN-GAP composite propellant composed of... Fig. 7.59 Burning rates and temperature sensitivity thereof for TAGN-GAP composite propellant composed of...
The thermodynamic potential defined by Tg/Mg is approximately the same for both TAGN-GAP and HMX-GAP composite propellants. [Pg.181]

Figure 7-29. Burning rate and temperature sensitivity of TAGN-GAP composite propellant composed of 1(0.2). Figure 7-29. Burning rate and temperature sensitivity of TAGN-GAP composite propellant composed of 1(0.2).
See other pages where TAGN-GAP propellant is mentioned: [Pg.103]    [Pg.224]    [Pg.225]    [Pg.103]    [Pg.224]    [Pg.225]    [Pg.94]    [Pg.181]    [Pg.182]    [Pg.103]    [Pg.224]    [Pg.225]    [Pg.103]    [Pg.224]    [Pg.225]    [Pg.94]    [Pg.181]    [Pg.182]    [Pg.223]    [Pg.223]    [Pg.223]    [Pg.180]    [Pg.180]    [Pg.181]    [Pg.93]   
See also in sourсe #XX -- [ Pg.94 ]



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