Aerospace Engineering > GATE 2013 > Orbital Mechanics
Consider the low earth orbit (LEO) and the geo synchronous orbit (GSO). Then
A
ΔV requirement for launch to LEO is greater than that for GSO, and altitude of LEO is lower than that of GSO
B
ΔV requirement for launch to LEO is lower than that for GSO, and altitude of LEO is lower than that of GSO
C
ΔV requirement for launch to LEO is greater than that for GSO, and altitude of LEO is greater than that of GSO
D
ΔV requirement for launch to LEO is lower than that for GSO, and altitude of LEO is greater than that of GSO

Correct : b

Similar Questions

Which of the following statements is/are correct about a satellite moving in a geostationary orbit?
#34 MSQ
At a point in the trajectory of a space vehicle moving about the Earth, the altitude above the mean sea level is 6400 km, and the speed with reference to a coor...
#47 MCQ
Consider an artificial satellite moving around the Moon in an elliptic orbit. The altitude of the satellite from the Moon's surface at the perigee is 25 km and...
#68 Fill in the Blanks

Related Topics

DeltaV LEO vs GSO LEO vs GSO orbital mechanics GATE Aerospace Engineering 2013 LEO altitude GSO altitude LEO ΔV GSO ΔV orbital mechanics aerospace LEO GSO comparison

Unique Visitor Count

Total Unique Visitors

Loading......