At an altitude of 5000 m the rocket's acceleration has increased to 6.9 m/s2 . What mass of fuel has it burned?

(a) The initial upward acceleration of the rocket is 6.0 m/s².

(b) The mass of the fuel that burned is 1,000 kg.

The given parameters;

(a) The acceleration of the rocket is calculated as follows;

T = mg + ma

(b) The mass of the fuel that burned is calculated as follows;

The mass of the fuel =

"Your question is not complete it seems to be missing the following information;"

1.9×104 kg rocket has a rocket motor that generates 3.0×105 N of thrust.

(a) What is the rocket's initial upward acceleration? Express your answer to two significant figures and include the appropriate units

(b) At an altitude of 5000 m the rocket's acceleration has increased to 6.9 m/s2 . What mass of fuel has it burned?

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1) Initial upward acceleration:

2) Mass of burned fuel:

Explanation:

1)

There are two forces acting on the rocket at the beginning:

- The force of gravity, of magnitude , in the downward direction, where

is the rocket's mass

is the acceleration of gravity

- The thrust of the motor, T, in the upward direction, of magnitude

According to Newton's second law of motion, the net force on the rocket must be equal to the product between its mass and its acceleration, so we can write:

(1)

where a is the acceleration of the rocket.

Solving for a, we find the initial acceleration:

2)

When the rocket reaches an altitude of 5000 m, its acceleration has increased to

The reason for this increase is that the mass of the rocket has decreased, because the rocket has burned some fuel.

We can therefore rewrite eq.(1) as

where

is the new mass of the rocket

Re-arranging the equation and solving for m', we find

And since the initial mass of the rocket was

This means that the mass of fuel burned is

jupiter

explanation:

it is so massive and has such a strong gravitational pull its likely prevented the formation of a planet between itself and mars in the asteroid belt

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