Final answer:
The acceleration of the rocket can be calculated using the equation a = T / m, where T is the thrust and m is the mass of the rocket. Substituting the given values, the acceleration is determined to be 26.67 m/s².
Step-by-step explanation:
In the given problem, a 6 kg model rocket burning fuel generates a thrust of 160 N. The thrust of the engines can be calculated using the equation:
T = m * a
Where T is the thrust, m is the mass of the rocket, and a is the acceleration.
Knowing the mass of the rocket, we can rearrange the equation to solve for acceleration:
a = T / m
Substituting the given values, we get:
a = 160 N / 6 kg = 26.67 m/s²
Therefore, the acceleration of the rocket is 26.67 m/s².