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相关概念视频

Circular Orbits and Critical Velocity for Satellites01:16

Circular Orbits and Critical Velocity for Satellites

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The Moon orbits around the Earth. In turn, the Earth (and other planets) orbit the Sun. The space directly above our atmosphere is filled with artificial satellites in orbit. One can examine the circular orbit, the simplest kind of orbit, to understand the relationship between the speed and the period of planets and satellites with respect to their positions and the bodies that they orbit.
Nicolaus Copernicus (1473-1543) first suggested that the Earth and all other planets orbit the Sun in...
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Rocket Propulsion in Empty Space - I01:13

Rocket Propulsion in Empty Space - I

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The driving force for the motion of any vehicle is friction, but in the case of rocket propulsion in space, the friction force is not present. The motion of a rocket changes its velocity (and hence its momentum) by ejecting burned fuel gases, thus causing it to accelerate in the direction opposite to the velocity of the ejected fuel. In this situation, the mass and velocity of the rocket constantly change along with the total mass of ejected gases. Due to conservation of momentum, the...
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Rocket Propulsion In Empty Space - II01:12

Rocket Propulsion In Empty Space - II

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The motion of a rocket is governed by the conservation of momentum principle. A rocket's momentum changes by the same amount (with the opposite sign) as the ejected gases. As time goes by, the rocket's mass (which includes the mass of the remaining fuel) continuously decreases, and its velocity increases. Therefore, the principle of conservation of momentum is used to explain the dynamics of a rocket's motion. The ideal rocket equation gives the change in velocity that a rocket...
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Schwarzschild Radius and Event Horizon01:21

Schwarzschild Radius and Event Horizon

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No object with a finite mass can travel faster than the speed of light in a vacuum. This fact has an interesting consequence in the domain of extremely high gravitational fields.
The minimum speed required to launch a projectile from the surface of an object to which it is gravitationally bound so that it eventually escapes the object’s gravitational field is called the escape velocity. The escape velocity is independent of the mass of the object. Merging the idea of escape...
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Escape Velocity01:26

Escape Velocity

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The escape velocity of an object is defined as the minimum initial velocity that it requires to escape the surface of another object to which it is gravitationally bound and never to return. For example, what would be the minimum velocity at which a satellite should be launched from the Earth's surface such that it just escapes the Earth's gravitational field?
To calculate the escape velocity, it is assumed that no energy is lost to any frictional forces. In practice, a satellite...
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Reduced Mass Coordinates: Isolated Two-body Problem01:12

Reduced Mass Coordinates: Isolated Two-body Problem

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In classical mechanics, the two-body problem is one of the fundamental problems describing the motion of two interacting bodies under gravity or any other central force. When considering the motion of two bodies, one of the most important concepts is the reduced mass coordinates, a quantity that allows the two-body problem to be solved like a single-body problem. In these circumstances, it is assumed that a single body with reduced mass revolves around another body fixed in a position with an...
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相关实验视频

Updated: May 31, 2025

Thermocapillary Convection Space Experiment on the SJ-10 Recoverable Satellite
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Thermocapillary Convection Space Experiment on the SJ-10 Recoverable Satellite

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由于空间物体重新进入空域,导致空域关闭.

Ewan Wright1, Aaron Boley2, Michael Byers3

  • 1Interdisciplinary Studies Graduate Program, University of British Columbia, Vancouver, BC, Canada.

Scientific reports
|January 23, 2025
PubMed
概括

失控的火箭体重新进入构成对飞机的碰撞风险越来越大. 当局面临着由于安全原因而关闭空域和航班延误造成的经济影响之间的困境.

科学领域:

  • 太空碎片 太空碎片
  • 航空安全航空安全
  • 风险评估 风险评估

背景情况:

  • 无人控制的太空物体重新进入太空,对空中的飞机构成碰撞风险.
  • 由于太空发射和空中交通增加,这种风险正在升级.
  • 国家当局可以在重新进入事件期间预防性关闭空域,影响运营.

研究的目的:

  • 量化火箭体重新进入影响不同空中交通密度的空域的概率.
  • 分析管理重新进入风险的当局所面临的安全和经济权衡.

主要方法:

  • 在不同的空域密度上对火箭体再进入事件的概率分析.
  • 基于空中交通水平的碰撞风险评估.

主要成果:

  • 靠近机场的高密度地区每年有0.8%的重返影响的机会.
  • 像美国东北部或北欧这样繁忙的空域地区每年面临高达26%的风险.
  • 碰撞风险和空域关闭的经济影响随着空中交通密度的增加而增加.

结论:

  • 国家当局面临着管理重新进入风险,平衡安全与经济后果的困境.

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  • 控制的重新进入海洋可以减轻风险,但超过2300个火箭体需要几十年来管理不受控制的重新进入.