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相关概念视频

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...
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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 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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PD Controller: Design01:26

PD Controller: Design

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In automotive engineering, car suspension systems often employ Proportional Derivative (PD) controllers to enhance performance. PD controllers are utilized to adjust the damping force in response to road conditions. A controller, acting as an amplifier with a constant gain, demonstrates proportional control, with output directly mirroring input.
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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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Optimization, Test and Diagnostics of Miniaturized Hall Thrusters
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实验室在PCB上的固体推进剂微推进器具有多模式推进能力.

Jeongrak Lee1, Seonghyeon Kim1, Hanseong Jo1

  • 1Department of Mechanical Engineering, Pohang University of Science and Technology, Pohang, Gyeongbuk 37673, Republic of Korea. annalee@postech.ac.kr.

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|August 7, 2024
PubMed
概括
此摘要是机器生成的。

一个新的共享室固体燃料微推进器,使用实验室印刷电路板 (PCB) 技术制造,为纳米/微卫星应用提供一致的推力和多种模式.

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科学领域:

  • 航空航天工程 航空航天工程
  • 材料科学 材料科学 材料科学
  • 纳米技术纳米技术

背景情况:

  • 在纳米/微卫星集群中对微推进器的需求不断增长.
  • 现有的固体推进剂微推进器在推力一致性,可扩展性和耐用性方面面临挑战.
  • 传统的基于MEMS的微冲击器制造的局限性.

研究的目的:

  • 提出和开发一种新的共享室固体推进器微推进器设计.
  • 为了解决不一致的推力,有限的模式和生产挑战的问题.
  • 为了利用实验室在印刷电路板 (PCB) 技术进行增强的微型冲击器制造.

主要方法:

  • 使用实验室在PCB和PCB表面安装技术设计和制造共享室微推进器.
  • 实施点火和燃烧实验以验证单元的运行.
  • 评估不同的操作模式,包括功率和连续推力.

主要成果:

  • 在指定的位置产生一致的推力.
  • 成功地适应多个推力模式 (动力和连续).
  • 通过PCB技术证明了增强的结构稳定性,可扩展性和大规模生产潜力.

结论:

  • 基于PCB的实验室共享室固体推进器微推进器为卫星推进提供了可行的解决方案.
  • 该设计克服了现有的微推进器的局限性,提供了更好的性能和可制造性.
  • 与推进和电子控制系统的集成显示了未来卫星任务的巨大潜力.