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Sustainer stage

Fig. 14.13 shows a typical example of a propellant grain for which the burning surface area ratio of the booster stage and sustainer stage is 2.18. The relahonship... [Pg.415]

TWrfB = CdbA, Pb for the booster stage rh s = CdsA Ps for the sustainer stage... [Pg.419]

The equilibrium chamber pressure during the sustainer stage (ps) is simply determined by Eq. (14.10) as... [Pg.419]

Fig. 14.18 A pair of photographs of the cross-section of propellant 2 (a) before combustion, and (b) after combustion interruption at the transition from booster stage to sustainer stage. Fig. 14.18 A pair of photographs of the cross-section of propellant 2 (a) before combustion, and (b) after combustion interruption at the transition from booster stage to sustainer stage.
See other pages where Sustainer stage is mentioned: [Pg.414]    [Pg.414]    [Pg.414]    [Pg.415]    [Pg.416]    [Pg.417]    [Pg.417]    [Pg.418]    [Pg.418]    [Pg.418]    [Pg.419]    [Pg.419]    [Pg.420]    [Pg.420]    [Pg.414]    [Pg.414]    [Pg.414]    [Pg.415]    [Pg.416]    [Pg.417]    [Pg.417]    [Pg.417]    [Pg.418]    [Pg.418]    [Pg.418]    [Pg.419]    [Pg.419]    [Pg.420]    [Pg.420]    [Pg.145]    [Pg.155]    [Pg.161]    [Pg.161]   
See also in sourсe #XX -- [ Pg.414 ]

See also in sourсe #XX -- [ Pg.414 ]



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