An earth-orbiting satellite has an elliptic orbit with a semimajor axis of 1.05 du where 1 du is equal to 1 earth radius. when the satellite is at the end of the semi-minor axis, it receives an impulsive velocity change (a fuel burn) just sufficient to place it on a parabolic escape trajectory. what is the magnitude of the velocity change? compute the answer indu/tu and then convert to km/s. an earth-orbiting satellite has an elliptic orbit with a semimajor axis of 1.05 du where 1 du is equal to 1 earth radius. when the satellite is at the end of the semi-minor axis, it receives an impulsive velocity change (a fuel burn) just sufficient to place it on a parabolic escape trajectory. what is the magnitude of the velocity change? compute the answer indu/tu and then convert to km/s.

i would say the answer is food.

hope this !

d₁ = displacement of tern from arctic to antarctic = 11000 miles

d₂ = displacement of tern from antarctic to arctic =   - 11000 miles

d = total displacement for the journey

total displacement for the journey is given as

d = d₁ + d₂

d = 11000 + (-11000)

d = 0 miles

t₁ = time of travel from arctic to antarctic = 3 months = 3 x 30 days = 90 days

t₂ = time of travel from antarctic to arctic = 3 months = 3 x 30 days = 90 days

t = total time of travel

total time of travel is given as

t = t₁ + t₂

t = 90 + 90

t = 180 days

average velocity is given as

average velocity = total displacement/ total time

v = d/t

v = 0/180

v = 0 miles/day

part 1: which substance has a higher solubility?

a

smallest amount left undissolved atall temps in table shown most has dissolved high sol'by