5 - 16 Usable SM RCS propellant remaining, lb 20 200 180 160 140 120 100 80 60 40 100 0 20 40 60 80 305 240 200 160 40 80 120 0 Onboard gaging, percent Ground elapsed time, hr Figure 5-3 SM RCS propellant profi le - quad B 280 Quad B
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Apollo 11 Flight Plan, Final - July 1, 1969 resources

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5 - 16 Usable SM RCS propellant remaining, lb 20 200 180 160 140 120 100 80 60 40 100 0 20 40 60 80 305 240 200 160 40 80 120 0 Onboard gaging, percent Ground elapsed time, hr Figure 5-3 SM RCS propellant profi le - quad B 280 Quad B

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