K2. 2.41The Pegasus launch vehicle reaches its second-stage burnout at an altitude of192 km, inertial velocity v = 5.49 km/s, and flight-path angle y = 25.8°. The launchvehicle then coasts in this orbit until it ignites its third stage when flight-pathangle decreases to 2.2°. Determine:a) Semimajor axis of the Pegasus orbit after second-stage burnout.b) Eccentricity of the Pegasus orbit after second-stage burnout.c) The altitude and velocity of the Pegasus launch vehicle when the third stage isignited.

Given parameters:r (altitude above Earth's surface): 192 kmv (velocity): 5.49 km/sλ (flight-path…

Answered: The Pegasus launch vehicle reaches its…

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Hi there, looks like c is incorrect because wouldn't you use the 1/2 gt2
T1 please help me with the answer and full solution
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