Which of these is not a part of in-plane orbit changes?

Change of inclination of the orbits

Hohmann transfer

Adjustment of perigee an apogee height

General coplanar transfer between circular orbits

Correct Answer : Change of inclination of the orbits

Explanation : When the satellite is launches, there’s often error in burnout altitude, speed, flight path angle and the exact orbit that was desired is not achieved. This is corrected by applying a small delta-v in the same plane to adjust the orbital parameters. The in-plane corrections include- Hohmann transfer, adjustment of perigee and apogee height, general coplanar transfer between circular orbits.

Recently Updated in Spaceflight Mechanics Questions

Which of these is not a type of an impulsive maneuver?

Energy change

Simple plane change

Adjustment of perigee and apogee height

Combined change of apsis altitude and plane orientation

Correct Answer : Option (A) : Energy change

Explanation : There are four types of single impulse maneuver-Adjustment of perigee and apogee height, simple rotation of the line of apsides, simple plane change and combined change of apsis altitude with plane orientation. There is no change in energy involved by applying single impulse.

What does non- impulsive maneuver mean?

Rockets with instantaneous bursts

Rocket fire short bursts for required delta-v

Maneuvers which are analyzed by Lambert�s equation

Rocket fires long bursts for long time for the required delta-v

Correct Answer : Option (D) : Rocket fires long bursts for long time for the required delta-v

Explanation : When the thrust applied by the rocket is done over a longer period to obtain the required delta-v, it is known as the non-impulsive maneuver. Unlike impulsive maneuver it does not involve applying impulse over a short period.

When the change in velocity represents a change in direction, what kind of maneuver is it called?

Pumping maneuver

Orbital raising maneuver

Cranking maneuver

Orbital lowering maneuver

Correct Answer : Option (C) : Cranking maneuver

Explanation : Each impulsive maneuver results in a velocity change of the spacecraft. This velocity change yield both magnitude and direction change of the velocity vector. When Δv represents a change in direction it is referred as a cranking maneuver.