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相关概念视频

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 Gravitational Field - I01:20

Rocket Propulsion in Gravitational Field - I

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Rockets range in size from small fireworks that ordinary people use to the enormous Saturn V that once propelled massive payloads toward the Moon. The propulsion of all rockets, jet engines, deflating balloons, and even squids and octopuses are explained by the same physical principle: Newton's third law of motion. The matter is forcefully ejected from a system, producing an equal and opposite reaction on what remains.
The motion of a rocket in space changes its velocity (and hence its...
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Rocket Propulsion in Gravitational Field - II01:03

Rocket Propulsion in Gravitational Field - II

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A rocket's velocity in the presence of a gravitational field is decreased by the amount of force exerted by Earth's gravitational field, which opposes the motion of the rocket. If we consider thrust, that is, the force exerted on a rocket by the exhaust gases, then a rocket's thrust is greater in outer space than in the atmosphere or on a launch pad. In fact, gases are easier to expel in a vacuum.
A rocket's acceleration depends on three major factors, consistent with the...
2.0K
Acceleration due to Gravity on Other Planets01:24

Acceleration due to Gravity on Other Planets

3.4K
The gravitational acceleration of an object near the Earth's surface is called the acceleration due to gravity. It can be measured by conducting simple experiments on Earth. However, such an experiment is impossible to conduct on the surface of other planets.
Astronomical observations are thus used to measure the acceleration due to gravity on other planets. This can be determined by observing the effect of a planet's gravity on objects close to it. The crucial factor that helps in this...
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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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Torque Free Motion01:15

Torque Free Motion

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The torque-free motion refers to the movement of a rigid body in space when no external torques are acting upon it. This type of motion can be observed in environments where there are no external forces or frictions, like in outer space. For example, a rotation of Mars in space is a torque-free motion. Mars is an axisymmetric object, meaning it has an axis of symmetry along which it rotates, designated as the z-axis. The rotating frame of reference is defined such that the center of mass of...
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相关实验视频

Updated: May 3, 2026

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters
12:22

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters

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引力拖拉机用于拖小行星.

Edward T Lu1, Stanley G Love

  • 1NASA Johnson Space Center, Mail Code CB, Houston, Texas 77058, USA. edward.t.lu@nasa.gov

Nature
|November 11, 2005
PubMed
概括

一个新的航天器设计使用重力来拖小行星,改变它们的轨道以保护地球. 这种方法是强大的,不受小行星组成或旋转的影响,提供了可靠的行星防御策略.

科学领域:

  • 行星科学 行星科学
  • 航空航天工程 航空航天工程
  • 天体动力学是指天体动力学.

背景情况:

  • 小行星撞击对地球构成重大威胁.
  • 目前的小行星偏移方法在小行星特性方面存在局限性.

研究的目的:

  • 为小行星轨道改变提出一个新的航天器设计概念.
  • 为行星防御提供基于重力的拖线方法.

主要方法:

  • 一艘航天器在小行星附近悬浮,利用其引力.
  • 推进器的废气向外导向,以避免表面相互作用.
  • 该方法旨在独立于小行星的物理特征.

主要成果:

  • 拟议的方法提供可控制的轨迹改变.
  • 该设计对小行星结构,表面特性和旋转状态不敏感.
  • 这种方法提供了一个强大的行星防御解决方案.

结论:

  • 重力拖线航天器概念为小行星偏移提供了一个可行的和可适应的战略.
  • 这种创新方法增强了行星防御能力,防止潜在的冲击威胁.

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