What is the setback of using the gravitational slingshot maneuver to send spacecraft to another planet?

Time consuming

Less economical

More fuel consumption

Limitation of correct alignment of planets

Correct Answer : Limitation of correct alignment of planets

Explanation : On of the major setbacks for using the gravitational slingshot is that there are very rare occurrences for the planets to align in way expected for the optimum slingshot to occur. It can take several years, decades to achieve a perfect alignment of the celestial bodies.
On the other hand, slingshot mostly accelerates the spacecraft thus making it less time consuming. And since it makes use of lesser fuel, it is ore economical.

Recently Updated in Spaceflight Mechanics Questions

What kind of trajectory is obtained if the satellite is launched from a place whose latitude is 30 deg

Arc trajectory

Co-axial trajectory

Coplanar trajectory

Non-coplanar trajectory

Correct Answer : Option (D) : Non-coplanar trajectory

Explanation : Coplanar trajectory only occurs when the launch is at a suitable condition where launch latitude matches the moon’s orbital inclination. This is a rare condition which occurs only at Cape Kennedy whose latitude for launch is 28.5 deg. When launches are done at any other location or when the suitable conditions is not met, it results in non-coplanar trajectory.

Which of these is not a constraint on lunar trajectories?

Phase of the moon

Accuracy tolerance

Launch site location

Rotation speed of the earth

Correct Answer : Option (D) : Rotation speed of the earth

Explanation : There are several constraints which carrying out lunar missions. These include-launch site location, accuracy tolerance, limited range of injection conditions, phase of the moon determining the lighting condition, direction of launch from a site.

What is the right ascension of launch point equal to?

Synodic time

Local sidereal time

East longitude

Greenwich sidereal time

Correct Answer : Option (B) : Local sidereal time