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Correct Answer : 1 km/s
Explanation : The change in velocity for the single impulse maneuver is always higher than 1km/s as there are no re- fueling stations in the space for the spacecraft, so the Δv has to be calculated beforehand to minimize propellant mass carried for the payload.
Correct Answer : Option (D) : Perigee and apogee of the final orbit
Explanation : When there is a Hohmann transfer, the smallest possible transfer ellipse occurs when the transfer takes place at either apogee of perigee of the final orbit which is at a point opposite to the terminating point.
Correct Answer : Option (C) : Hohmann transfer
Explanation : When the initial and final orbits are circular, the optimal maneuver is called a Hohmann transfer. This transfer consists of two tangential velocity impulses which I applied at the initial and final radius.
Correct Answer : Option (C) : When impulse is applied tangential
Explanation : For a coplanar maneuver, multi-impulse maneuver is very efficient. The minimum velocity impulse is achieved when the impulse is applied in the same direction of initial and final velocity vector. This is known as tangential impulse.