I don't understand the apparent weight thing
Sum of F witha arrow to the right = ma (the "a" has a arrow at the top pointing to the right)
then it says "so that T-mg=ma"
T= mg+ma
The T's and g's and a's have the arrow.
Could some one please explain this.
I have no clue what it is.
Also this question
A model rocket has a pre launch mass or 85 g, of which 25g is solid propellant. It is able to deliver a trhust of 3.8N for a period of 2.8s. Assuming that hte rocket is fired directly up, determine
1) initial rate of accleration and g force
b) the final rate of acceleration and g force just prior to exhaustion of the fuel
In the solution for B) the "g" force
9.8 + 54
---------
9.8
the 54 being the final acceleration
My question is why are you adding 9.8 isn't it the gravity value at the specific altitude?, I know it's not significant but still.
Also the question states it's fired directly up, if it wasn't what would be different?
Thanks
Sum of F witha arrow to the right = ma (the "a" has a arrow at the top pointing to the right)
then it says "so that T-mg=ma"
T= mg+ma
The T's and g's and a's have the arrow.
Could some one please explain this.
I have no clue what it is.
Also this question
A model rocket has a pre launch mass or 85 g, of which 25g is solid propellant. It is able to deliver a trhust of 3.8N for a period of 2.8s. Assuming that hte rocket is fired directly up, determine
1) initial rate of accleration and g force
b) the final rate of acceleration and g force just prior to exhaustion of the fuel
In the solution for B) the "g" force
9.8 + 54
---------
9.8
the 54 being the final acceleration
My question is why are you adding 9.8 isn't it the gravity value at the specific altitude?, I know it's not significant but still.
Also the question states it's fired directly up, if it wasn't what would be different?
Thanks
Last edited: