An empty spacecraft weighs 250,000 N on earth and carries 700,000 N of propellant. The spacecraftlands on Mercury, where the acceleration due to gravity is 3.7 m/s2. If the craft used 2/3 of its fuelmass to get to Mercury, how much thrust (in Newtons) will be required to lift-off from the planetif the minimum thrust is equal to the spacecraft weight?

10 points! will mark brainiest! in a heat engine if 1,000 j of heat enters the system and the piston does 500 j of work, what is the final internal energy of the system if the initial energy was 2,000 j 1: write the equation 2: list out your known variables 3: plug the numbers into the equations 4: solve 5: write your solution statement that includes initial energy and final energy added you so much!

Both independent and dependent clauses

How do i solve this physics problem?