Solving for Lunar Landing Craft Thrust

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    Lunar Thrust
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Homework Help Overview

The discussion revolves around calculating the thrust required for a lunar landing craft to safely touch down on the moon's surface. The craft's mass, gravitational acceleration, and descent velocity are provided, and participants are exploring the necessary calculations to determine the thrust needed to reduce the craft's velocity to zero upon landing.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning, Problem interpretation

Approaches and Questions Raised

  • Participants discuss the forces acting on the lunar lander, including gravity and thrust, and question how to apply Newton's Second Law. There are attempts to derive the necessary acceleration and thrust using kinematic equations and force balance.

Discussion Status

Some participants have provided guidance on using Newton's Second Law and kinematic equations to find the required thrust. There is ongoing exploration of the calculations, with some expressing uncertainty about the correctness of their results and others suggesting verification of the approach.

Contextual Notes

Participants note variability in the problem's numerical values and express concerns about potential errors in calculations. There is a recognition that the thrust must be less than the gravitational force for the landing to be successful.

onyxorca
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Homework Statement



A 8.73 × 103-kg lunar landing craft is about to touch down on the surface of the moon, where the acceleration due to gravity is 1.60 m/s2. At an altitude of 217 m the craft's downward velocity is 16.5 m/s. To slow down the craft, a retrorocket is firing to provide an upward thrust. Assuming the descent is vertical, find the magnitude of the thrust needed to reduce the velocity to zero at the instant when the craft touches the lunar surface.

http://edugen.wiley.com/edugen/courses/crs2216/art/qb/qu/c04/EAT_12257263467150_5449420724903514.gif

Homework Equations



v^2=v0^2+2ax

The Attempt at a Solution



Fthrust=Fg? mg=ma?
 
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What is the needed acceleration to bring the velocity down to zero over the given height?
How many forces act on the lander as it is coming down?
Can you write Newton's Second Law?
 
Hello onyxorca,

As a first step you have to figure out which forces act on the rocket. Then you have to use the general equations for x(t) and v(t).
 
F=ma

the forces are gravity and thrust.

btw the mass is 8.73 × 10^3 kg.

the acceleration is 0=16.5^2+2a217 and a = -0.627304 m/s^2 ? where do i go from there?
 
Use Newton's Second Law. Find an expression for the net force (the sum of all the forces) and set it equal to mass times acceleration.
 
Fthrust - Fg = ma?

so F - 8730*1.6 = 8730*-0.627304

F=8491.64 N?
 
F_thrust -F_g = ma is correct! :smile:

Now you need to find out the value of a.

For that use the general equations for x(t) and v(t):

v(t) = a*t + v_0

x(t) = 1/2*a*t^2 + v_0*t + x_0
 
rogerbacon said:
Now you need to find out the value of a.

OP found the acceleration in Posting #4. The answer is OK.
 
well appearantly 8491 isn't right...
 
  • #10
I checked the numbers and I checked the method. The answer should be correct. If someone (or a computer program) says that it is not, then you need to take your solution to the person who assigned this problem and ask him/her where the error is.
 
  • #11
V0=V^2+2ax find a

F=mg-ma=m(g-a)

i finally got it right, had trouble realizing that the thrust is smaller than gravitational force and i made mistakes when putting in the scientific digits but i finally got it.
 
  • #12
onyxorca said:
F=mg-ma=m(g-a)

This is the right answer. What number do you get when you plug in?
 
  • #13
well the numbers in the problem changes every time so i wouldn't know if this is right but i got the right answer for that time.

in this case though it's probably F = 8.73E3 (1.6+.627304) = 19444.4 N because it's Fg-Fthrust, not the other way around.
 
  • #14
I get the same number.
 

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