Calculating Momentum Change for Rocket Course Alteration

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To calculate the momentum change for a rocket altering its course, one must consider the total mass of the rocket and its velocity. The rocket, with a mass of 3700 kg and a velocity of 110 m/s, aims to change direction by 35 degrees using expelled gases at 1900 m/s. The key to solving this problem lies in determining the momentum added in the perpendicular direction to achieve the desired course alteration. Understanding the momentum expelled per second is crucial for calculating the necessary gas mass to be expelled. A detailed breakdown of these calculations will lead to the solution.
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Hey, I've been having trouble with the following question, and I've tried all I can think of and still can't get it. Your help is much appreciated.

"A rocket with a total mass of 3700kg is traveling in outer space with a velocity of 110m/s towards the sun. It wishes to alter its course by 35.0 degrees, and can do this by firing its rockets briefly in direction perpendicular to its original motion. If the rocket gases are expelled at a speed of 1900m/s, how much gas mass must be expelled?"

I already know the answer, its just a matter of getting to the answer that I have trouble with. A detailed explanation in other words.
 
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Hi daxter17! Welcome to PF! :smile:

Hint: how much momentum is being expelled per second? :wink:
 
It doesn't say really that's the question right out of the textbook. Wish I could help more but I'm stuck myself.
 
daxter17 said:
"A rocket with a total mass of 3700kg is traveling in outer space with a velocity of 110m/s towards the sun. It wishes to alter its course by 35.0 degrees, and can do this by firing its rockets briefly in direction perpendicular to its original motion.

ok, so how much momentum is added in that perpendicular direction? :smile:
 
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