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TAGN-GAP Composite Propellants

Fig.4.22 Specific impulse, adiabatic flame temperature, and molecular mass of combustion products for TAGN-GAP composite propellants. Fig.4.22 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.
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...
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).
The thermodynamic potential defined by Tg/Mg is approximately the same for both TAGN-GAP and HMX-GAP composite propellants. [Pg.181]

See other pages where TAGN-GAP Composite Propellants is mentioned: [Pg.223]    [Pg.180]    [Pg.223]    [Pg.180]    [Pg.223]    [Pg.223]    [Pg.180]   
See also in sourсe #XX -- [ Pg.223 ]

See also in sourсe #XX -- [ Pg.223 ]

See also in sourсe #XX -- [ Pg.180 ]



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