Answer:
26 lbf
Explanation:
The mass of the satellite is the same regardless of where it is.
The weight however, depends on the acceleration of gravity.
The universal gravitation equation:
g = G * M / d^2
Where
G: universal gravitation constant (6.67*10^-11 m^3/(kg*s))
M: mass of the body causing the gravitational field (mass of Earth = 6*10^24 kg)
d: distance to that body
15000 miles = 24140 km
The distance is to the center of Earth.
Earth radius = 6371 km
Then:
d = 24140 + 6371 = 30511 km
g = 6.67*10^-11 * 6*10^24 / 30511000^2 = 0.43 m/s^2
Then we calculate the weight:
w = m * a
w = 270 * 0.43 = 116 N
116 N is 26 lbf
I think it’s manufacturing
Location of the class depends on satiation
Answer:
LAOD = 6669.86 N
Explanation:
Given data:
width![= 25 mm = 25\times 10^{-3} m](https://tex.z-dn.net/?f=%20%3D%2025%20mm%20%3D%2025%5Ctimes%2010%5E%7B-3%7D%20m)
thickness ![= 6.5 mm = 6.5\times 10^{-3} m](https://tex.z-dn.net/?f=%3D%206.5%20mm%20%3D%206.5%5Ctimes%2010%5E%7B-3%7D%20m)
crack length 2c = 0.5 mm at centre of specimen
![\sigma _{applied} = 1000 N/cross sectional area](https://tex.z-dn.net/?f=%5Csigma%20_%7Bapplied%7D%20%3D%20%201000%20N%2Fcross%20sectional%20area)
stress intensity factor = k will be
![\sigma_{applied} = \frac{1000}{25\times 10^{-3}\times 6.5\times 10^{-3}}](https://tex.z-dn.net/?f=%5Csigma_%7Bapplied%7D%20%3D%20%5Cfrac%7B1000%7D%7B25%5Ctimes%2010%5E%7B-3%7D%5Ctimes%206.5%5Ctimes%2010%5E%7B-3%7D%7D)
![= 6.154\times 10^{6} Pa](https://tex.z-dn.net/?f=%3D%206.154%5Ctimes%2010%5E%7B6%7D%20Pa%20)
we know that
![k =\sigma_{applied} (\sqrt{\pi C})](https://tex.z-dn.net/?f=k%20%3D%5Csigma_%7Bapplied%7D%20%28%5Csqrt%7B%5Cpi%20C%7D%29)
[c =0.5/2 = 2.5*10^{-4}]
K = 0.1724 Mpa m^{1/2} for 1000 load
if
then load will be
![Kc = \sigma _{frac}(\sqrt{\pi C})](https://tex.z-dn.net/?f=Kc%20%3D%20%5Csigma%20_%7Bfrac%7D%28%5Csqrt%7B%5Cpi%20C%7D%29)
![\sigma _{frac} = 41.04 MPa](https://tex.z-dn.net/?f=%5Csigma%20_%7Bfrac%7D%20%3D%2041.04%20MPa)
![load = \sigma _{frac}\times Area](https://tex.z-dn.net/?f=load%20%3D%20%5Csigma%20_%7Bfrac%7D%5Ctimes%20Area)
![load = 41.04 \times 10^6 \times 25\times 10^{-3}\times 6.5\times 10^{-3} N](https://tex.z-dn.net/?f=load%20%3D%2041.04%20%5Ctimes%2010%5E6%20%5Ctimes%2025%5Ctimes%2010%5E%7B-3%7D%5Ctimes%206.5%5Ctimes%2010%5E%7B-3%7D%20N)
LAOD = 6669.86 N
Answer:
What is the difference Plastic vs elastic deformation
Explanation:
The elastic deformation occurs when a low stress is apply over a metal or metal structure, in this process, the stress' deformation is temporary and it's recover after the stress is removed. In other words, this DOES NOT affects the atoms separation.
The plastic deformation occurs when the stress apply over the metal or metal structure is sufficient to deform the atomic structure making the atoms split, this is a crystal separation on a limited amount of atoms' bonds.