/* 
   Name: Group #058
   Author: Anna Reese
           Odessa Gomez
   Description: In a 2-stage rocket, when given payload and the exaust velocity
                find the fuel necessary to reach Low Earth Orbit(LEO)
*/
#include 
#include 
#include 
#include 

float fuelwt(double payload_wt,double exhaust_vel){  //function which finds the fuel weight when given
                                                     //payload and exhaust velocity
                                                     
//***********declarations************

float v1, v2, ratio, payload, a, b, c, d, e, f;      //variables needed for finding fuel

double x1, x2, r1, r2;                               // doubles in order to use them in logrithems