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8.107: a) For t < 0 the rocket is at rest. For ≤ t ≤ 8 .40 is valid, and<br />

v( t) = ( 2400 m s) ln( 1 ( 1−<br />

( t /120 s)<br />

)).<br />

At t = 90 s, this speed is 3.33 km/s, and this is also<br />

the speed for t > 90 s.<br />

0 90 s, Eq. ( )<br />

b) The acceleration is zero for t < 0 and t > 90 s. For 0 ≤ t ≤ 90 s, Eq. (8.39) gives,<br />

with dm<br />

2<br />

20 m/s<br />

= −m0<br />

120 s, a =<br />

dt<br />

( 1−( t /120 s)<br />

) .<br />

c) The maximum acceleration occurs at the latest time of firing, t = 90 s, at which time<br />

2<br />

20 m/s<br />

2<br />

the acceleration is, from the result of part (a), ( ) = 80 m/s , and so the astronaut is<br />

1−<br />

90 /120<br />

subject to a force of 6.0 kN, about eight times her weight on earth.

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