Answer:
<u>The correct answer is r = ∛GM*T²/4π²</u>
Step-by-step explanation:
Let's rewrite the formula to find the period of orbit of a satellite around a planet, to solve for r, this way:
T^2=(4pi^2/GM)r^3
T² = (4π²/GM) * r³
r³ = T²/ (4π²/GM)
r³ = T² * GM/4π²
r³ = GMT²/4π²
∛r³ = ∛GM*T²/4π²
r = ∛GM*T²/4π²
<u>The correct answer is r = ∛GM*T²/4π²</u>
Geggggggggggggggggggggggggggggggggggggggggggggggggggggggggggg like yuhh
350 because of the concert I’m just kindling I need points
Answer:
<u><em>1 cup</em></u>
Step-by-step explanation:
<em>Total</em>
<em>= 1/4(2) + 1/2</em>
<em>= 1/2 + 1/2</em>
<em>= 1 cup</em>
<em></em>
<em>Hope it helps.</em>
<em>;)</em>
<em><3</em>
