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関連する概念動画

Rocket Propulsion in Empty Space - I01:13

Rocket Propulsion in Empty Space - I

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 rocket's...
Rocket Propulsion In Empty Space - II01:12

Rocket Propulsion In Empty Space - II

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 experiences by...
Rocket Propulsion in Gravitational Field - I01:20

Rocket Propulsion in Gravitational Field - I

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...
Rocket Propulsion in Gravitational Field - II01:03

Rocket Propulsion in Gravitational Field - II

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 equation for the...
Heart Sounds01:15

Heart Sounds

Heart sounds are generated by the turbulence in blood flow due to the closing of heart valves. These sounds are best perceived slightly away from the valves, where the blood flow disseminates the sound.
Auscultation is the process of listening to these internal body sounds using a stethoscope. The heart produces four types of sounds, but only two—S1 and S2—can usually be heard with a stethoscope.
S1, also known as the "lub" sound, is caused by the closure of atrioventricular (A-V) valves at the...
Impact: Problem Solving01:26

Impact: Problem Solving

In an experiment conducted during a Mars mission, a rover propels a projectile with an initial velocity, and the projectile rebounds after colliding with the Martian surface. To ascertain the maximum height attained by the projectile after this collision, the known restitution coefficient and acceleration due to gravity are employed.
By designating the launch point as the origin and utilizing kinematic equations, the vertical component of the projectile's velocity at the point of impact is...

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関連する実験動画

Updated: Jun 21, 2026

Bringing the Visible Universe into Focus with Robo-AO
10:35

Bringing the Visible Universe into Focus with Robo-AO

Published on: February 12, 2013

宇宙でアポロロケットの音が聞こえる.

D Cotten, W L Donn

    Science (New York, N.Y.)
    |February 12, 1971
    PubMed
    まとめ

    アポロロケットからの低周波音波がバミューダで検出された. 高空から発するこれらの信号は,稀化した大気における衝撃形成理論によって説明される.

    科学分野:

    • アコースティクス アコースティクス
    • 航空宇宙工学は,航空宇宙工学である.
    • 大気物理学 大気物理学

    背景:

    • 低周波音現象は,高速の大気現象によって発生することがあります.
    • 以前の研究では,ロケット打ち上げからの音響信号が調査されていますが,高空からの音源は依然として理解が不十分です.

    研究 の 目的:

    • アポロロケットの打ち上げ中に記録された低周波音の起源と特性を調査する.
    • これらの音響信号が,大気の衝撃波理論によって説明できるかどうかを判断する.

    主な方法:

    • アポロロケットの通過中にバミューダの三方配列によって記録された音響データの分析.
    • 信号特性 (一貫性,速度,到着時間,周波数) とロケット軌道のデータとの比較.
    • 稀化した大気における衝撃形成に対する運動理論の応用と,ガスダイナミクスの衝撃理論.

    主要な成果:

    • 一貫した低周波音信号は,アポロロケットが188kmの高さで打ち上げられたときと一致して,複数回記録された.
    • 信号は高超音速で,配列全体で一貫した特徴 (外観,周波数,到着時間) を示した.
    • 観測された表面圧力変動は,高い高度での衝撃形成の理論的モデルと一致していました.

    さらに関連する動画

    Measurement and Analysis of Atomic Hydrogen and Diatomic Molecular AlO, C2, CN, and TiO Spectra Following Laser-induced Optical Breakdown
    09:40

    Measurement and Analysis of Atomic Hydrogen and Diatomic Molecular AlO, C2, CN, and TiO Spectra Following Laser-induced Optical Breakdown

    Published on: February 14, 2014

    Simulating Imaging of Large Scale Radio Arrays on the Lunar Surface
    06:14

    Simulating Imaging of Large Scale Radio Arrays on the Lunar Surface

    Published on: July 30, 2020

    関連する実験動画

    Last Updated: Jun 21, 2026

    Bringing the Visible Universe into Focus with Robo-AO
    10:35

    Bringing the Visible Universe into Focus with Robo-AO

    Published on: February 12, 2013

    Measurement and Analysis of Atomic Hydrogen and Diatomic Molecular AlO, C2, CN, and TiO Spectra Following Laser-induced Optical Breakdown
    09:40

    Measurement and Analysis of Atomic Hydrogen and Diatomic Molecular AlO, C2, CN, and TiO Spectra Following Laser-induced Optical Breakdown

    Published on: February 14, 2014

    Simulating Imaging of Large Scale Radio Arrays on the Lunar Surface
    06:14

    Simulating Imaging of Large Scale Radio Arrays on the Lunar Surface

    Published on: July 30, 2020

    結論:

    • 記録された低周波の音は,高空でのアポロロケット車両に決定的に起因する.
    • 運動理論とガスダイナミクスを組み合わせたアプローチは,観測された音響現象と表面圧力効果をうまく説明します.