document.write( "Question 957164: The mass (in Mg) of the fuel supply in the first-stage booster of a rocket is m = 135 - 6t - t^2, where is the time ( in s) after launch. When does the booster run out of fuel \n" ); document.write( "
Algebra.Com's Answer #584922 by Fombitz(32388)![]() ![]() You can put this solution on YOUR website! \n" ); document.write( " \n" ); document.write( " \n" ); document.write( "Only positive t makes sense here. \n" ); document.write( " \n" ); document.write( " |