B. 75 m/s
C. 1700 m/s
D. 2400 m/s
Spacecraft will be moving in 1700 m/s.
Option C
The diameter of the moon is 3500 km and the free fall acceleration at the surface is given as
The radius will be half of the diameter of the moon that can be written as:
By the application of the equation for orbit speed, we get
The spacecraft is moving at approximately 1700 m/s.
The speed of the spacecraft can be calculated using the formula for the orbital speed of an object:
V = sqrt((G * M) / r)
Where V is the velocity, G is the gravitational constant (approximately 6.67 x 10^-11 N m²/kg²), M is the mass of the moon (approximately 7.35 x 10^22 kg), and r is the radius of the moon plus the altitude of the spacecraft.
Plugging in the known values, we have:
V = sqrt((6.67 x 10^-11 N m²/kg²) * (7.35 x 10^22 kg) / (3.5 x 10^6 m + 200 m))
Calculating the square root of this expression gives us approximately 1700 m/s.
#SPJ3
She can monitor her practice run times to see if they are decreasing.
Answer: a
Explanation:
The displacement covered in a certain time will decrease.
The speed of the object will stay constant.
The velocity of the object will change.
Given:
P1 = 400 kPa
T1 = 110 K
T2 = 235K
Required:
P2
Solution:
Apply Gay-Lussac’s law where P/T = constant
P1/T1 = P2/T2
P2 = T2P1/T1
P2 = (235K)(400kPa) / (110K)
P2 = 855 kPa