thrust
The ________- to- weight ratio varies continually during a flight.
Rocket vehicle Thrust
________- to- weight ratio vs specific impulse for different propellant technologies.
instantaneous thrust
The ________- to- weight ratio of a vehicle varies continually during operation due to progressive consumption of fuel or propellant and in some cases a gravity gradient.
thrust
The ________- to- weight ratio of a rocket improves as the propellant is burned.
thrust
The ________- to- weight ratio and wing loading are the two most important parameters in determining the performance of an aircraft.