The amount of thrust needed to get to Mars varies depending on the spacecraft's design, weight, and mission profile. Generally, it requires a spacecraft to achieve a velocity of around 24,600 miles per hour (39,600 kilometers per hour) to escape Earth's gravity and enter a trajectory towards Mars. The thrust generated during launch must overcome Earth's gravitational pull and atmospheric drag. Additionally, precise calculations are necessary for trajectory adjustments during the journey to ensure successful arrival at Mars.
Only robot probes can land on mars. But there are some evidence that is needed to be cleared
The amount of fuel needed to travel to Mars and back depends on various factors such as the spacecraft design, propulsion system, payload weight, and trajectory. For a mission like NASA's Mars Rover, Curiosity, it required around 2000 pounds (900 kg) of fuel for the journey to Mars. The return trip would require a similar amount of fuel.
Smaller. Much smaller.
Impossible to say. We do not have that much information about Mars.
Not much gas at all, as Mars is a rocky planet with not much of an atmosphere.
That depends on the weight and design of the aircraft.
687 Earth Days.
Not possible...
Thrust Capacity is how much thrust it can take :D
The amount of thrust needed for takeoff depends on several factors, including the aircraft's weight, design, and environmental conditions like altitude and temperature. Generally, an aircraft requires thrust that exceeds its weight to become airborne, typically around 1.2 to 1.3 times the weight of the aircraft. For commercial jets, this often translates to tens of thousands of pounds of thrust, while smaller aircraft may require significantly less. Each aircraft's specifications provide detailed thrust requirements for safe takeoff.
The amount of thrust depends on the power of the engine
The amount of thrust needed to launch a rocket varies depending on the size, weight, and destination of the rocket. On average, rockets require anywhere from hundreds of thousands to millions of pounds of thrust to overcome Earth's gravity and achieve orbital velocity. For example, the Saturn V rocket used during the Apollo missions had a maximum thrust of 7.6 million pounds.
thrust
To fly, only thrust and lift are needed. The F-16s jet engines provide the thrust, and its wings provide the lift.
there is not much difference between thrust anf force...its just that thrust is the force acting perpendiclular to the surface thrust will always be either equal or greater than force.
Only robot probes can land on mars. But there are some evidence that is needed to be cleared
Mars rotates in 24 hours 40 minutes.