
A certain rocket maintains a horizontal attitude of its axis during the powered phase of its flight at high altitude. The thrust imparts a horizontal component of acceleration of 20ft/sec 2 , and the downward acceleration component is the acceleration due to gravity at that altitude, which is g = 30 ft/sec 2 . At the instant represented, the velocity of the mass center G of the rocket along the 15º direction of its trajectory is 12,000 mi/hr. For this position determine
Text Solution
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Sol. We observe that the radius of curvature appears in the expression for the normal component of acceleration, so we use n– and t-components of the total acceleration are obtained by resolving the given horizontal and vertical accelerations into there n- and t-components and then combining.

From the figure we get
a n = 30 cos 15º – 20 sin 15º = 23.8 ft/sec 2 a t = 30 sin 15º + 20 cos 15º = 27.1 ft/sec
2 We may now compute the radius of curvature from
[a n = v
2 / ρ ] ρ =
=
= 13.01 (10 6 ) ft Ans.
The rate at which v is increasing is simply the t-component of acceleration.
[
= a t ]
= 27.1 ft/sec 2 Ans.
The angular rate
of line GC depends on v and ρ and is given by
[v = ρ
]
= v/ ρ =
= 13.53(10 –4 ) rad/sec . Ans.
With unit vectors e n and e t for the n- and t-directions, respectively, the total acceleration becomes
a = 23.8e n + 27.1e t ft/sec 2 Ans.
Helpful Hints:
1. Alternatively we could find the resultant acceleration and then resolve it into n- and t-components.
2. To convert from mi/hr to ft/sec., multiply by
=
which is easily remembered, as 30 mi/hr is the same as 44 ft/sec.
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