A rocket weighing 300,000 N is taking off from Earth with a total thrust of 460,000 N at an angle of 20 degrees, as shown in the image below. What is
the approximate vertical component of the net force that is moving the rocket
away from Earth?
20°
Vertical
Componenti
of Net Force 1
Thrust
460,000 N
Weight
300,000 N
O
A. 168,000 N
B. 215,000 N
C. 132,000 N
D. 105,000 N

Iwould sure like to answer your question but i honestly just don’t know

What does the start look like

If the heat engine is a perfect carnot cycle engine, thenefficiency = (t2-t1)/t2   where t1=temperature of cold reservoir ( ° k) = 135            t2=temperature of hot reservoir ( ° k)   = 325thereforeefficiency = (t2-t1)/t2 = (325-135)/325 = 0.5846 = 58%  note: this is the theoretical maximum efficiency of a perfect heat engine.   real-life engines do not achieve this value.