Question 4 Name and describe the transformation of Figure Q to Figure R.
Translation. Figure Q slid 6 units to
the right to Figure R
Translation Figure Q slid 4 units to
the right to Figure R.
Reflection Figure Q was flipped
over the y-axis, the line of reflection.
Fig Q
Fig R
Reflection Figure Q was flipped
over the x-axis, the line of reflection,

Aspacecraft can attain a stable orbit 300 kilometers above earth if it reaches a velocity of 7.7 kilometers per second. the formula for a rocket's maximum velocity v in kilometers per second is vequalsminus0.0098tplusc ln upper r, where t is the firing time in seconds, c is the velocity of the exhaust in kilometers per second, and r is the ratio of the mass of the rocket filled with fuel to the mass of the rocket without fuel. find the velocity of a spacecraft whose booster rocket has a mass ratio of 20, an exhaust velocity of 2.1 km/s, and a firing time of 15 s. can the spacecraft achieve a stable orbit 300 km above earth?