Spaceflight Mechanics - Two-Body Mechanics Quiz(MCQ)

A)
TV Broadcasting
B)
Fixed Wireless
C)
Weather Forecasting
D)
Global Positioning System

Correct Answer :   Fixed Wireless


Explanation : Fixed Wireless is a type of communication that occurs between two fixed devices or between two fixed locations. An example of fixed wireless is communication between a computer and a Wi-Fi router. All other options are well implemented through satellites.

2 .
What is the tangential velocity of a satellite moving in a circular orbit at a height of 5250 km above the surface of Earth? The standard gravitational parameter of Earth is 398,600 km3/s2. The radius of Earth is 6378 km.
A)
5.85 km/s
B)
6.01 km/s
C)
7.91 km/s
D)
11.1 km/s

Correct Answer :   5.85 km/s


Explaination : Given,
Distance between Earth and satellite (r) = 5250 + 6378
= 11,628 km
Standard gravitational parameter of Earth (μ) = 398,600 km3/s2
Since, gravitational attraction between Earth and satellite = centrifugal force of the satellite, we can derive,
Tangential velocity of satellite (V) = (μ/r)1/2
= (398,600/11,628)1/2
= 5.85 km/s

3 .
The standard parameter of Earth is 398,600 km3/s2, distance between Earth and Mars is 225 x 106 km, force of gravitational attraction between Earth and Mars is 6.39 x 1023 N. What is the standard gravitational parameter of Mars? Given, universal gravitational constant is 6.67408 × 10-11 m3 kg-1 s-2.
A)
12,890 km3/s2
B)
34,567 km3/s2
C)
42,647 km3/s2
D)
78,901 km3/s2

Correct Answer :   42,647 km3/s2


Explaination : Given,
Force of attraction between Earth and Mars (F) = 6.39 x 1023 N
Distance between Earth and Mars (r) = 225 x 106 km
Standard Gravitational Parameter of Earth (μE) = 398,600 km3/s2
Universal gravitational constant (G) = 6.67408 × 10-11 m3/(kg.s2)
From Newton’s law of gravitation,
Mass of Mars (m) = (Fr2)/μE
= (6.39*1023*(225*106)2)/(398,600*109)
= 6.39 x 1023 kg
Standard Gravitational Parameter of Earth (μM) = G.m
= 6.67408*10-11*6.39*1023
= 42,647 km3/s2

4 .
What is the force of attraction between earth and moon? Given, distance between earth and moon is equal to 384,400 km, standard gravitational parameter of earth is equal to 398,600 km3/s2 and mass of the moon is equal to 7.348 x 1022 kg.
A)
1.771 x 1026 N
B)
1.982 x 1017 N
C)
2.042 x 1012 N
D)
6.192 x 1017 N

Correct Answer :   1.771 x 1026 N


Explaination : Given,
Standard gravitational parameter of earth (μ) = 398,600 km3/s2
Mass of moon (m) = 7.348 x 1022 kg
Distance between earth and moon (r) = 384,400 km
Force of attraction (F) = (μ.m) / (r)2
= (398,600 x 7.348 x 1022) / (384,400)2
= 1.982 x 1017 N

5 .
What is the acceleration due to gravity at a height of 10 km from the surface of earth? The acceleration at the MSL is 9.81 m/s2 and the radius of earth is 6378 km.
A)
9.68 m/s2
B)
9.78 m/s2
C)
9.99 m/s2
D)
10 m/s2

Correct Answer :   9.78 m/s2


Explaination : Given,
Acceleration due to gravity at MSL (g0) = 9.81 m/s2
Radius of Earth (RE) = 6378 km
Height above the surface (h) = 10 km
Acceleration due to gravity at 10 km (g) = g0 / (1 + h / RE)2
= 9.81/(1+10/6378)2
= 9.78 m/s2

6 .
What is the resultant instantaneous acceleration of a rocket with a combined mass of 1.98 x 106 kg at that instant. Total thrust produced by the rocket is 31 x 106 N.
A)
3.25 m/s2
B)
4.2 m/s2
C)
5.85 m/s2
D)
7.1 m/s2

Correct Answer :   5.85 m/s2


Explaination : Given,
Thrust (T) = 31 x 106 N
Mass of rocket (m) = 1.98 x 106 kg
Resultant Force (F) = T-mg
= 31*106-(1.98*106*9.81)
= 11.57 x 106 N
From Newton’s second law,
Resultant instantaneous acceleration (a) = F/m
=(11.57*106)/(1.98*106)
= 5.85 m/s2

A)
Euler problem
B)
Kepler problem
C)
Two-body problem
D)
N-body problem

Correct Answer :   N-body problem


Explanation : When we have o predict and analyze the motion of multiple celestial objects in the sky as a result of their gravitational forces acting on each other, we use N-body problem to solve the dynamics.

A)
True
B)
False
C)
Can Not Say
D)
None of the above

Correct Answer :   False


Explanation : In N-body problems, where there’s mutual forces between several celestial bodies, the net external force and torque are both zero due to the Newton’s third law.

A)
N
B)
2N
C)
3N
D)
6N

Correct Answer :   6N


Explanation : In case of N-body problem, there are 3N second order differential equations which results in 6N motion variables.

A)
N
B)
2N
C)
3N
D)
6N

Correct Answer :   3N


Explanation : The N-body problem has 3N degrees of freedom which makes use of 3N second order differential equations for finding the position of the particle.

A)
Orbits are circular
B)
Mass of one of the bodies is negligible
C)
Their positions don’t change over time t
D)
The gravitational force exerted on each other cancels out

Correct Answer :   Mass of one of the bodies is negligible


Explanation : In case of restricted three-body problem, it is a simplified version of three-body problem where it is assumed that one of the masses is almost negligible compared to the other two. This m1 and m2 move in Keplerian orbit which is unaffected by m3.

12 .
What order of magnitude does the earth’s oblateness affect the gravitational forces?
A)
10-2 g’s
B)
10-3 g’s
C)
10-4 g’s
D)
10-5 g’s

Correct Answer :   10-3 g’s


Explaination : There are certain variations introduced due to the earth’ oblateness effect. This force is of the order 10-3 g’s. Newton’s law is only applicable for spherical objects.

A)
One-body problem
B)
Two-body problem
C)
Three-body problem
D)
Five-body problem

Correct Answer :   One-body problem


Explanation : The simplest case of the N-body problem is a case which has only one body. In the entire space, there lies only one body with mass m. It experiences no force, acceleration and moves with a constant velocity.

A)
Result converge
B)
It is time consuming
C)
Lack of initial condition data
D)
Closed form solution does not exist

Correct Answer :   Closed form solution does not exist


Explanation : N-body problems are usually chaotic for initial conditions and require numerical method to compute the result. Analytical results cannot be obtained wince there no closed form solution existing. So far, two body problems and restricted 3-body problem can be solved.