S: Thrust vs Gravity & F22 Raptor

In summary, the F22 raptor has a 2:1 thrust to weight ratio, allowing it to climb vertically and hover. However, this ratio is not enough to overcome the force of gravity and achieve continuous acceleration. At high altitudes, the presence of oxygen decreases and affects engine output, altering the thrust to weight ratio and acceleration. The concept of acceleration can be understood in terms of gravity and the effects of air resistance on the aircraft's speed.
  • #1
AstroNOT
2
0
The F22 raptor has an approximate 2:1 thrust to weight ratio. It can climb vertically and stand on its tail in a hover.

Vertical acceleration is given by: Thrust - Drag - Weight = mass * acceleration (aka gravity). The opposing force to thrust involves an acceleration due to the force of gravity which is roughly equal to 9.8 m/s/s. So a 2:1 thrust ratio, though fun, cannot overcome the force of gravity i.e. accelerate continually -- in which case the craft would reach escape velocity which is in excess of 11 km/s or in the vicinity of mach10.​

Please advise about any misinformation here. As well as the mechanics that keep this craft from accelerating beyond 70k feet. How does one conceptualize per second per second acceleration? Distance per second is conceivable. Acceleration is observable. But the designation escapes me.

Thanks for any advice.
AstroNOT
 
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  • #2
That paragraph doesn't make a whole lot of sense. At a 2:1 thrust ratio, a plane will accelerate vertically until drag slows the acceleration and then will decelerate as the engines lose thrust at high altitude.

I'm not sure I understand your question in the last part. m/s/s is the units of acceleration.
 
  • #3
At the very least, it shouldn't really be too hard to concieve of the units of acceleration. Meters per second per second means how many (meters per second) it gains every second.
 
  • #4
Acceleration is the change of velocity per second. For example in the case of gravity, acceleration indicates a change in velocity of 32 ft/sec each second.

For constant vertical acceleration, the jet aircraft would require constant atmosphere. As the aircraft climbs, the presence of oxygen diminishes and dramatically affects engine output. Combustion efficiency depends on cool dense atmosphere. High altitude flight affects turbine engines and decreases thrust, altering the thrust to weight ratio and acceleration.
 
  • #5
Conceptionalise acceleration in terms of gravity. For example, you might say the raptor has 2 g's of acceleration. It can overcome the force of gravity (which means to hover), it just can't overcome the force of air resistance pressing against it at a few times the speed of sound or beyond. Also, it can't fly without the atmosphere, which (ignoring limited fuel supplies) is the only reason helicopters can't just slowly inch their way to outer space.
 

1. What is the difference between thrust and gravity?

Thrust is the force that propels an object forward, while gravity is the force that pulls an object towards the center of the Earth.

2. How does thrust affect the flight of an F22 Raptor?

Thrust is crucial for the flight of an F22 Raptor, as it provides the necessary force to overcome the weight of the aircraft and maintain steady flight.

3. What is the maximum thrust of an F22 Raptor?

The maximum thrust of an F22 Raptor is approximately 35,000 pounds, which allows the aircraft to reach supersonic speeds and perform high-speed maneuvers.

4. How does the F22 Raptor's thrust-to-weight ratio affect its performance?

The F22 Raptor's high thrust-to-weight ratio allows it to accelerate quickly and maintain high speeds, making it a highly maneuverable and agile aircraft.

5. How is the thrust of an F22 Raptor generated?

The thrust of an F22 Raptor is generated by two powerful engines, each with a thrust vectoring nozzle that can redirect the exhaust gases to provide vertical thrust for takeoff and landing, as well as enhanced maneuverability.

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