paulb203
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- Homework Statement
- Booster rockets can be reused if they land safely. One way to slow a booster for landing is by firing its engine again. Now, thrust pushes opposite the direction the booster is moving. This technique is called propulsive landing.
Determine the thrust needed to propulsively land the booster described below.
A 25,000kg booster rocket is falling. It experiences a gravitational pull of 245,000N.
The booster's engine fires for 13 seconds before landing, slowing the booster from a velocity of
172 m/s to 0 m/s over that time.
- Relevant Equations
- a=v-u/(t)
a=Fnet/m
a=v-u/(t)
a=0-172/(13)
a=approx -13m/s^2
*
a=Fnet/m
-13=Fnet/25000
Fnet=-13(25000)
Fnet=-3250000N
Fg+Fth=-325000N
Fth=-325000-245000
Fth=-670000N
Any hints as to where have I gone wrong?
a=0-172/(13)
a=approx -13m/s^2
*
a=Fnet/m
-13=Fnet/25000
Fnet=-13(25000)
Fnet=-3250000N
Fg+Fth=-325000N
Fth=-325000-245000
Fth=-670000N
Any hints as to where have I gone wrong?